Quick viewing(Text Mode)

A Comparative Evaluation of Five Tire Traction Models

A Comparative Evaluation of Five Tire Traction Models

A Comparative Evaluation of Five Traction Models

INTERIM DOCUMENT 6

by John T. Tielking Naveen K. Mital

January 1974

Highway Safety Research Institute / University of Michigan

SHEET UM-HSRI-PF-74-2 1 1 4. 'I'it It and Suht lt ic 5. Report D~te A COMPARATIVE EVALUATIOH OF FIVE TIRE TRACTION XODELS / January 1974

7. Autlior(s) 8. Performing Organization Rep:. J.T. Tielking and N.K. Mital No. UM-HSRI-PF-74-2 9. i'crform~nr,OrK~niz3rion hame and AdJres.i 10. Project ,T~sic.lock Unit :;o. Highway Safety Research Institute - University of Michigan 11. Contract/Granr So. Huron Parkway and Baxter Road Ann Arbor, Michigan 48105 12. Sponsor~ni:Or ani:.irldn Yare and ,Address 13. Type of Report & Pe,*od Motor ~efiicfeElanufacturers Association Covered 320 New Center Building Detroit, Michigan 48202 14.

15. Supplcmentary Notes r Interim Document 6: Tire Traction Characteristics Affxting Vehicle Performance 16. Absrracrs - Five tire nodeis which have the capability 07; simulating tire traction iorczs and aligning moment ic response to combincd longitudind and lateral slip (braking and steering) dre evaluated in a new set of c~ordinatzsdesignea to simplify the closed-form algebraic traction force and momnt expressions. The traction responses of the five ti;e models are corpared and the effects of various assumptions made in the derivation nf each model are discussed. A chapter is devoted to tire testing for model input data. Digital computer prog~arlsare included.

\7c. COSATI Fir iJ/Group I 18. Ava~labillr~Statement 19. Securit: Ciass (This 21. 10. of Pages Report) UhXIElITED L'~CI.A

A COFIPARATII'E EITALUATION OF FIVE TIRE TRACTION hlODELS

John T. Tielking Naveen K. ;\Iital

Project 329180

Tire Traction Characteristics Affecting Vehicle Performance

Document 6

January 1974

Sponsored by

The Motor Vehicle Manufacturers Association The study of tire traction yodels contained in this document was conducted as part of an ongoing tire research project entitled "Tire Traction Characteristics .lffecting Vehicle Performance,'' sponsored by the Motor \-ehicle blanufacturers .Association. I primary objective of this research project is to develop a mathematical model capable of predicting the significant mechanical performance characteristics of the pneumatic tire from basic design and operating variables.

The research reported herein \{as conducted to gain a thorough understanding of the development and operation of recently published tire traction models. :I systematic set of definitions for the operating variables describing tire orientation, motion, and shear force generation was developed in the framework of a system of tire and contact region coordinates defined to facilitate tire model study.

Four published tire models are recast in this new coordinate system and rederived xcith the common set of operating variable definitions.

fifth tire model is derived by a change of pressure distribution.

The tire model responses to a common set of tire characterizing data and operating variable ranges are compared and the effects of various as~unptio~s~.ade during model derivation are identified.

Secavse cf the variations found in the response of the five tire modeis to the same input data, comparison with experimental data was not attempted in this document. The next stage of this tire research effort will be concerned with a quantitative validation of the various tire models with measured tire traction data. TABLE OF CONTENTS

IYTRODUCTION ...... 1 Coordinate Systems ...... 1 General Kinematics ...... 5 Yodel Definition ...... 10 FORCE AND ?IO3IENT EQUATIONS ...... :7 HSRI-NBS-I ...... 21 HSRI.NBS.11 ...... 27 Goodyear Model ...... 44 Sakaiblodel ...... 55 HSRI-NBS-I11 ...... 69 TIRE TESTING FOR MODEL INPUT DATA ...... 77 Standing Tire Tests ...... 78 Rolling TireTests ...... 84 MODEL RESPONSE COMPARISOSS ...... 91 Traction Force Comparisons ...... 93 Aligning Moment Comparisons ...... 103 REFERENCES ...... 107 SY?IBOLS AND TERMINOLOGY ...... 108

.APPENDIX I . MODEL RESUhIES ...... 111

APPENDIX I1 . SUMMARY OF FORhIULAS ...... 113

.APPENDIX I11 . LOCI OF ADHESION LIhlIT POINTS ...... 126

APPENDIX IV . DIGITAL COPIiPUTER PROGRAMS ...... 137

INTRODUCTION

The models analyzed in this document were recently developed for the simulation of tire traction characteristics produced by tire-road interfacial shear forces. Some of the models have the capability of simulating aligning morent in addition to the traction forces. Although the publication of a tire xraction model always includes a comparison of its response wit3 measured tire data, there is no discussion on the relative merits of the new model compared with previous ones. This should not be con- sidered a defect in the literature as each model, in attempting to simulate certain aspects of tire behavior, contains a number of simplifying and sometimes indefensible assumptions. It should be recognized that a tire model is, of necessity, designed with a particular application in mind. This document is not written to declare one model superior over all others, but to present all of the models in a common format and to compare the response of each model to the others with the objective of identifying the effects of the various assumptions made during derivation. It is hoped that this document will facilitate the task of sifting through the literature to determine an adequate tire traction model for a particular application.

COORDINATE SYSTEMS

It is unfortunate that no standardized coordinate system suitable for tire traction work has been agreed upon. A tire axis system has been adopted by SAE [I]1 for inclusion in a l~i~uresin brackets indicate literature references on page 107. standardized vehicle dynamics terminology. This vehicle-oriented tire axis system ignores tire deformation and presumes a point rather than finite contact area. The SAE axis system, ~cllich originates at a hypothetical "center of tire contact," will be slightly modified in this document for use as a reference frame in the description of tire orientation, motion, and resultant traction force components.

For the study of tire traction, which involves a finite contact region whose location (with respect to the rigid wheel) and area are dependent upon tire operating variables, a separate coordinate system must be defined for the description of events taking place in the contact region. Since the contact region distortions associated with tire traction are very complex, it is important to adopt a contact coordinate system which will facilitate the derivation of traction equations and minimize their complexity.

The contact coordinates which are introduced in Figure 1 result from a study of many tire models. They considerably simplify the description of tire contact distortion and shear force generation.

The models analyzed in this document have been rederived in this new set of coordinates.

Figure 1 depicts an inclined tire rolling at a a. -. Poirt C, rn rigure l, lies on the road surface at the center of tire

3 CC?~~C*_"as Ccf!->e6. 'by $?i? 1-. -1:e :$,heel diameter passing through

C is inclined from vertical at an angle y.

/ "The center of tire contact is defined to be the intersection of the wheel plane and the vertical projection of the wheel axis onto the road plane. Figure 1. 'Tire coordinates (x,y, z) and contact coordinates (C ,Q) * Steady-state rolling of a uniform tire is presumed so that

it will not be necessary to distinguish between moving and inertial

coordinates. The tire coordinate system (x,y,z) originates at point C with x-y in the road plane and the z-axis vertical upward.

The \(heel velocity components ix and 1' are positive in the Y directions of the x and y axes. The slip angle a, measured from the x-axis to the direction of travel, is positive as shown in

Figure 1. Except for orientation (z-axis positive upward) the tire coordinate system (x,y,z) in Figure 1 is equivalent to the S-4E

tire axis system (X', Y', Z' in Fig. 1 of [I]). The slip angle a and the inclination angle y are SAE positive.

The contact coordinates (5,~)originate on the carcass equator at the point directly above the leading edge of the free-rolling contact area. The 5-axis runs rearward along the carcass equator and is allo~~edto deform with it. For the models considered in this document, the carcass equator is presumed flat and rigid in the contact region although able to translate laterally and longitudinally. The contact coordinates will translate with the carcass; the 5-2 plane remaining parallel with the road.

TCe deformation of the tread rubber with respect to the tire carcass ~cillbe described in the 5,~coordinate system. The lefornatlon of the carcass with respect to the center of tire contact is given by the relaticnship of the contact coordinates

(c,7) to the tire coordinates (x,y). The use of an independent contact coordinate system (5,~)thus allows separation of the influence of the tread rubber from the influence of carcass compliance on tire traction. \,c IOI. i t y vr\cto~.V. trti rc liiot ion is proclncccl 11)' constr~lirl i njj

the wheel planc to move at an angle n to the direction 01 travcl.

The travel velocity then has two components in the x,y coordinate system defined in the previous section. The longitudinal component,

V x = Vlcosa, is composed of the wheel rolling velocity Vr 2nd the velocity Ycx produced by longitudinal elastic slip and sliding in the contact region. The lateral component, 1. Y = /Vjsinn, is due entirely to lateral elastic slip or sliding and is generally termed the lateral slip velocity V C Y . The tire slip velocity vector, Vc shown in Figure 2, is defined by the slip velocity components VcX and V cy .

Figure 2. Kinematics of tire motion with braking applied. It is important to distinguish between the terms slip and sliding as used in tire terminology. Slip is here defined as tire motion not due to rolling. Trio independent phenomena contribute to slip. Perhaps the least-understood (in the kinematic sense) contribution is elastic deformation in the for1:ard part of the contact region. The tire carcass and attached tread comprise a highly deformable structure. As braking is applied to the rolling tire, the contact region moves rear~iardand the tire material entering contact begins to elongate. The elongation of the contacting material contributes a slip speed Vcx which becomes a certain percentage of the longitudinal velocity \lx. In the forward part of the contact region, the elastic deformation is produced by the tread elements adhering to the road surface. However, a point is reached where the available force is insufficient to balance the elastic deformation force and sliding begins con- tributing to the slip speed as the elongation contribution is reduced. Fure sliding with velocity V exists at the rear of the CX contact region. The contact deformations during braking are clearly seen in the photographs shown in Figures 7.2.60-62 of reference

121

The preceding discussion concerns straight ahead motion. If the tire is moving at a slip angle a, as shown in Figure 1, a l~.teralco-?orient of velocity arises which is due purely to slip. The elastic deformation is indicated by the path of the tread equator contact line shown dotted in Figure 1. In the adhesion area, the equator contact line parallels the direction of motion. 11s slitling hcgins, the trc:id cc1u:ttor hegins to returri to its undeformed position. The net result of this unsymmetric contact

region distortion is lateral tire motion with velocity Vcy.

When the tire is free-rolling, the rolling velocity is equal

to the wheel plane velocity Vx.

Vr = v X (free-rolling) (11

It is advantageous to define an effective rolling radius Re as

the ratio of the free-rolling velocity to the wheel spin velocity

S2.

R V (free-rolling) e

Experiments show that the effective rolling radius lies somewhere between the static loaded and unloaded radii. With the definition

of effective rolling radius, the rolling velocity for all braking

and driving torque applications can be determined from the

resulting spin velocity.

When braking is applied, the longitudinal velocity and the

rolling velocity are reduced by a certain amount each instant in time. Due to elastic deformation and sliding in the contact region, V decreases by a lesser amount. The difference is the X longitullinal slip velocity Vcx shown in Figure 2 at a certain instant in time. If driving torque is applied, elastic deformation and sliding cause the rolling velocity to exceed the longitudinal velocit~~ and lTcx becomes negative.

It is convenient to define a parameter s as the fraction of X longitudinal velocity which indicates the amount of braking or driving torque applied.

This parameter, called the longitudinal slip parameter, may exhibit the following range of values.

= 1 locked wheel I 1 < 1 braking traction

< 0 driving traction

3). use of Eq-uations (4) and (3), the definition of sX may be expressed as

Also useful is Equation (6) obtained by eliminating Vx from Equations (4) and (5). Analogous to the longitudinal slip parameter, the lateral slip parameter s is defined to be Y

- s Vcy/Vx = tana Y = where I' is the lateral slip velocity shown in Figure 2. Elimina- cY ting V from Equations (4) and (5), and substituting the resulting CX expression for V in Equation (7) results in the following useful X equation.

The slip velocity magnitude Vc = ]Vc 1 is computed from the components Vcx and V CY'

Introducing Equations (6) and (8) into the above gives the slip velocity magnitude as a fraction of the rolling velocity. -4s the wheel is locked (s 1,\TrO), the slip velocity X approaches the travel velocity and full sliding develops in the contact region. At lockup:

V = \? (from Equation (4)) CX X

17 = 1' (always) cY Y

V, = V, = v where VS is the sliding velocity vector.

IIODEL DEFINITION

The models derived in this document represent the by an array of elastic rectangular blocks attached radially to an elastic or rigid ring. The ring represents the tire carcass and may be rigidly attached to the mounting rim or separated from the rim by a spring foundation which permits lateral and longi- tudinal carcass motion to be simulated. In Figure 3, the carcass

Figure 3. Tire model: rectangular tread elements attached to an elastically supported deformable ring of bending stiffness EI. 10 ring, which has bending stiffness EI, moves on foundation springs of stiffness Kx and K . The tread blocks have infinitesimal 1.' volume in the contact region but undergo finite shear L1eformntions parallel to the road. Their longitudinal and lateral stiffnesses are kX and kV. The stiffness parameters KX, K and kx, k have Y ).' the units of force/length 3 .

The shear deformation of the single array3 of tread elements is con viently described in the 5,~contact coordinate system as shown in Figure 4.

Contact Entry Point

Figure 4. Braking/cornering deformation of tread element attached at B.

In time t, the base point R of a tread element will move into the contact region a longitudinal distance 5 determined by the rolling velocity Vr.

5 Deformation (and shear stress) is averaged across the tire tread. The resulting kinematic and force expressions will depend only on 6. If there is braking, the contacting tip A, which moves relative to iiith the wheel plane velocity 1,will cover an additional distance u as indicated in Figure 4. The displacement of point Al from the axis n is

Eliminating time from Equations (10) and (11) gives an expression for the longitudinal displacement u.

In terms of the longitudinal slip speed given by Equation (4),

The relative lateral velocity of contacting tip A is V c>- . In time t, this point is displaced laterally a distance v = -VCY t. Using Equation (10) to eliminate time gives an expression for the

Note that u and v depend only on the contact coordinate 5. The preceding analysis presumes that point A does not slide ~kyith respect to the road surface. From experimental observation, the contacting tip should describe a path parallel to the ;$heel. traveling velocity vector V. That it will do this is easily shown by writing the tangent angle of the dashed line path in Figure 4.

When the tangent of the angle 8 made by AB with the carcass equator is written with Equations (13) and (14),

it is seen that the deformed tread element AB in adhesion with the road is parallel to the slip velocity vector Vc.

In the adhesion region, the deformations u and v are produced by static friction with a limiting coefficient po. The components and q of the static friction force required to produce these 9, Y displacements depend upon the longitudinal and lateral stiffnesses of the element. 9, k V Since - = kTY CY , the static friction force vector rill not 9, X CX oppose the slip speed vector Vc unless the tread element stiffnesses are equal (kx = ky).

The right-hand sides of Equations (15) and (16) represent the components of linear elastic force developed in a tread element.

At any point in the adhesion region, the magnitude of the static friction force required to balance the elastic force is

The ir~asimum static friction available from a particular tire-road co~ilbinationdepends upon the limiting friction coefficient p 0 and the vertical contact pressure distribution q (5) which is assumed Z to be uniform in the 0 direction. The friction force requirement, computed by Equation (17), increases linearly as shown in Figure 5 until

. . ~f lih-i~hdef nes the 11n~11LL,5 a' the adhesion region. The tread element displacements Figure 5. Jlaximum static friction force P q, (6,) on tread element at Ca, the limit of adhgslon. are maximum at the adhesion limit which is located by evaluating Equation (17) at Sa.

Substituting (18) and (19) into (15) and (16) and the resulting expressions for q and q into the above, allows the adhesion limit X Y to be expressed as For a uniform contact pressure distribution, p = const.,

is used in Equation (20). For nonuniform contact pressures given by closed form expressions (such as parabolic), it may be possible

to solve Equation (20) for 5 a by rearrangement. In the case of arbitrary contact pressures, iteration of Equation (20) will be

necessary to obtain the adhesion limit 5 a . The preceding analysis is common to all linear element tire models since deformation behavior in the adhesion region is well known from observations of a tire rolling over a glass plate. By presuming linear elastic tire behavior the shear force generated at the road surface in the adhesion portion of the contact region can be easily computed. The situation is considerably more complicated in the sliding region where the sliding friction force rather than adhesive constraint governs the tire deformation. In the sliding region, one must presume a friction force and then compute the resulting displacements based on structure stiffnesses. This is directly opposite to the straightforward procedure followed in t4e adhesion region. The success or failure of a tire model is

in t.irect prcoortion to skill in approximating sliding region

Sekzx-fnr, I:OliCE ANTI MOMENT IIQU,IZTT ONS

'I'llc ridvantages o f using the two coorcli~l:ltc sys tcms (t i rc anil

contact) described earlier will now become apparent. The length

of the contact region as well as its location with respect to the

tire mounting rim varies with the tire operating conditions. L~' 1- 4 is convenient to define the non-sii;~ conract icrlgzi~. I, on :hi

carcass equator to uhich the <,r, coordinates are attached. 8y

presuming uaiform behavior laterally (across the finite contact width), the distributed contact shear forces qx and q ?' are defineC as functions of 5 only which is taken as the independent variable.

The resultant traction force components, F, and F Y' transmitted to

the tire mounting rim, are now obtained via the follo\qing integrals:

where w is the contact width.' The minus signs appear in Equations

(21) and (22) because Fx and F Y (applied to the tire by the road)

are referred to the tire coordinate system.

4 This is the contact length of the free-rolling tire at zero slip angle.

v 3 The contact region is seldom rectangular; L and w are representative dimensions. If the rigid carcass is elastically supported, as pr-sumed h). some tire models, the preceding traction forces may cause longitudinal

and lateral translations

which depend upon the carcass foundation stiffnesses Kx and K Y . The carcass translation for combined braking and cornering is shown in Figure 6.

I Rigid Carcass

y y

Figure 6. Sign convention for traction forces and moment. Following the sign convention given in Figure 6, the aligning moment expression may be written

which, with the aid of Equations (21-24), becomes

Due to the nonuniform distribution of the shear forces a and 'N and the carcass translations ti and ?, the resultant traction q~' forces are not necessarily colinear with the x and >I axes as shoii,~ in Figure 6. The traction forces Fx and F may be offset certain Y distances Ax and O from the wheel center as ;hewn in Figure Y 7.

Figure 7. Positive sign convention for traction force offsets ex and 1 Y . hloment equilibrium about the center of tire contact is expressed by

For straight ahead operation, F =IL,=Oand no aligning moment is ?', generated. For free-rolling at a slip angle, F =O which reduces X the moment equation to

The length Bx is frequently called the "pneumatic trail." It can

3c ;>ositive or negative depending on the tire operating conditions.

In the adhesion region, 5'5a, the shear forces qx and q Y are considered by all tire models in this document to be linearly distributed according to Equations (15-16) derived earlier The shear forces and displacements in the sliding region, 5,; .'a9 are approximated in a different manner by each of the follolting models discussed individually.

HSRI -NBS- I [3]

This model presumes tread eleme~~tdefor~~ation irL t;*e s l-z-.:- region to be uniform with the magnitude atTained at ;se ;L?~--G:J,. limit [=c Thus a '

vhere us and vS are the displacement components in the sliding region.

To sustain these displacements, the shear-stress components i; the sliding region are required to be qx = k u and q k v X S ?' - y s . The stress distribution over the entire contact region, sho1,cn In

Figure 8, implies a single friction coefficient p. This model considers p to be a linearly decreasing function of sliding speed according to

11 = p (1 - AI') 0 S S \$-here.A is an experimentally determined speed sensitivit). 5 coefficient and Figure 8. Deformation and stress ?resumed by HSRI-NBS-I modei.

it .;.~oulci he noted that here no distinction is made between slip

c . ., (1 slj6inq speed or static and dynamic friction. This is a

I-.ecess ary consecluence of prescribing the deformation (Equations i2F) and (2s)) beyond the adhesion limit. The adhesion limit is comnxted. by using u from Equation (30) instead of p in Equation 0

In the lateral direction, the integration of Equation (22) gives

If adhesion is complete,

Adhesion will be complete for small values of Vcx and V CY ' The use of Equations (6) and (8) permits the adhesive traction forces, (33) and (35), to be written in the following way.

The braking and cornering traction stiffnesses, Cs and Ca, are defined for complete adhesion according to

and. Carrying out the required operations on Equations (36) and (37)

yields

These parameters, which represent the slopes of the traction force

curves ps.ssing through the zero slip point, are easily determined

from experimental tire data. It is convenient to express the

traction forces in terms of Cs and Ca.

The HSRI-NBS-I model presumes the vertical contact pressure

distribution, qZ, to be uniform over the contact region. Thus, at the adhesion limit, where FZ is the tire load. The use of this assumption and

Equations (6), (8), (40), and (41) allows Equation (31) to be written as the adhesion fraction

where the friction coeffficient p varies with sliding speed as given by Equation (30).

For braking at a positive slip angle a, as illustrated in

Figure 1, the slip parameters sx and s = tana are positive. The Y traction forces computed by Equations (42) and (43) will be negative and generally oppose the direction of travel, decelerating the vehicle.

For locked wheel braking (sx=l), the adhesion fraction (45) vanishes and the traction forces become (on combining (45) with (42) and (43))

For straight ahead (s =0) locked wheel braking, the lateral force Y vanishes and the longitudinal force becomes simply During locked wheel travel, the sliding velocity equals the travel velocity V. The friction coefficient, considered to vary with sliding velocity, is then

The sliding region approximations made in the development of this model do not allow a reasonable equation for aligning moment to be derived by integration of Equation (25). The traction force calculations, (42) and (43), however, agree well with experimental data.

This model uses the limiting coefficient of static friction, to define the limit of the adhesion region. The limit of adhesion is given by Equation (20), written below in terms of the slip parameters s and s X Y .

In the sliding region, the available friction drops to the level of the dynamic coefficient p which is considered to be linearly related to sliding speed by Equation (30) used with the

HSRI-NBS-I model.

Instead of prescribing tread deformation in the sliding region, as was done in deriving the HSRI-NBS-I model, the shear stress in the sliding region will be recognized as having the magnitude pqZ and a direction6 opposing that of the sliding velocity. The tread deformation in the sliding region then depends on the longitudinal and lateral tread stiffnesses kx and k . Y

(sliding)

where, referring to Figure 9,

6 Due to tread pattern and preferential pavement surface direction, the sliding shear force may not be directed exactly opposite to the sliding velocity. This phenomenon can be accounted for by using anisotropic friction coefficients px and p as is done by the Sakai model discussed later. Y Figure 9, Deformation and stresses in HSRI-NBS-I1 model with instantaneous transition.

(full sliding, Vc=\Js) (52) v qy = pqzsinO = CY - uqz 5

For kx < k and Vcx < V the deformation and stresses will be Y CY' as shown in Figure 9.

The abrupt shift from adhesion to sliding produces a displace- ment discontinuity at c=ca (see Fig. 9). This discontinuity is unacceptable and indicates the existence of a finite transition region between adhesion and fully developed sliding. The accommodation of the transition region is a major contribution of the HSRI-NBS-I1 model. In passing through the transition region, a deformed tread element gradually changes its length and orientation. The sllenr force vector similarly changes its length and orientation in passing from geometrically constrained static friction to limiting dynamic friction generated during fully developed sliding. Finite transition behavior for kx > k is illustrated in Figure 10. Y

Figure 10. HSRI-NBS-I1 model with finite transition.

4t the adhesion limit, 5=5,, the incipient sliding speed + = O \

g,

Figure 11. Translation of fully sliding element CD for a definition of the transition region.

showing that the interior angles at A, C' and D' add up to 180'. k v -1 vs -1 y a Angle at C': 180" - (tan - - tan Us x a

Sum of angles: 180"

The factor A, which indicates the separation of the vertices at

A and Dl, may be determined from the slope of side Act.

After equating these expressions and solving for A,

kxUaVs - kuv A = ysa k -k u v (X Y) a a

From Equations (13) and (14),

with 5, given by Equation (20), and from Equations (51) ar,d (52), A is found to be independent of rolling velocity Vr.

In this expression, V = V + (Vcy)' since the translated S C =f(vCx)' element is in fully developed sliding. Referring to Figure 11, ,he transition length is seen to be

t = (A - l)(va cots - u a ) = (A-l)ca

The limit of the transition region is

3lultiplying Equation (54) for h by Equation (50) for ca results in an expression for the transition limit

1 1 d(k xV cx)' + (k YV CY )' 5, = uqz (Ss) (l-Sx) (F + F) x Vd(k s )2 + (ks )2 S XX YY which can be simplified by the use of Equations (6) and (8) to yield Recognizing that VS = Vc, Equation (9) can be used to write the sliding boundary in terms of the slip parameters.

This expression should be compared with Equation (50) as rewritten below.

A transition region must be considered only if the operating variables are such that Ss > 5. If 5, -< Sa, instantaneous transition from adhesion to steady-state sliding will be assumed.

If 5 > L, the entire contact region is in adhesion and there is a - no difference between the HSRI-NBS-I1 and HSRI-NBS-I models. It is possible to find > L in which case (if 5,

The transition region displacements, ut and vt, are presumed to be linearly decreasing during the transition from adhesion to fully developed sliding (Figure 12). The displacement components, line~rin 5, are now written by referring to Figure 12. Figure 12. Linear approximation of deformation and stress in the transition region.

Having prescribed the transition region displacements, the transition region shear stress components must be

(transition) (62)

These will decrease linearly to the sliding stress components given by Equations (52).

The shear stress distribution over the entire contact region may now be assembled. If the tire operating conditions are such that all three regions exist (Sa < tS < L), then cd -ALJ'

n n V) ALP - '.n N > CY 7 The resultant traction forces are obtained by summing the contributions from each region, viz.,

where, for a uniform contact pressure distribution qZ = FZ/wL,

The traction stiffnesses, Cs and Ca, given by Equations (40) and (41) have been used to simplify the above expressions. The transition forces Fxt and F are zero if 5 > 5, (then set Yt a 5, = 5,). The fully developed sliding forces FxS and F are YS zero if ts -> L (then set tS = L). The traction forces may be expressed in terms of slip parameters by using Equations (59) and (60) for Es and Ea, and the following expressions

For small values of slip, the contact will be entirely adhesive. In this case,

which is the result given by the HSRI-NBS-I model.

For locked wheel braking (sx = I), the adhesion and transition regions vanish. Setting Ea = 5, = 0 in Equations (66) and (67), the locked wheel traction forces are found to be

as well as the shear force distribution given by Equations (63). The total aligning moment is given by Equation (25) as rewritten below.

1j.h ere

After performing the integrations with the assumption of a uniform

contact pressure distribution, qz = FZ/wL, the contribution of each region to the total aligning moment is found. The traction stiffnesses, Cs and Cay given by Equations (40) and (41) have been used to simplify the above aligning moment expressions.

The transition region moment, Mzt, is zero if 5, 5, (then set = The sliding moment is zero if ts > L (then set 5 S Ea) - It is possible to have E > L, in which case there is 5, = L). a - neither a sliding nor a transition region and 5, = L, indicating complete adhesion, should be used in evaluating Equations (72). The aligning moment may be expressed in terms of the slip parameters in the same manner as the traction forces FX and F . Y For small values of slip, the contact is entirely adhesive and the aligning moment is given by Introducing the slip parameters sx and s into Equation (72) for Y M za and using Equations (68), the HSRI-NBS-I1 aligning moment for entirely adhesive contact is

For locked wheel braking (sx = I), Ss = 5, = 0 and Equation (71) reduces to

Using Equations (69) and (72) written in terms of slip parameters results in the HSRI-NBS-I1 aligning moment for fully sliding contact.

For the free-rolling tire at a small slip angle a, the aligning moment given by Equation (74) reduces to (with s = tanaza) Y The lateral force, in this situation, is given I)y the second of

1:quations (08).

It is now possible to compute a definite value foT the free-

rolling pneumatic trail R X by substituting Equations (77) and (78) into Equation (27).

(free-rolling)

The HSRI-NBS-I1 model thus predicts the free-rolling pneumatic trail to be one-sixth of the non-slip contact length. The lateral traction force resultant is located behind the wheel center as sho~in in Figure 13 and tends to align the wheel with the direction of travel.

Figure 13. Free-rolling pneumatic trail in for linear

tire traction models at small sl.ip angle ri. This result, valid for any7 free-rolling lateral motion which retains completely adhesive contact, is common to all models which treat the tire as a linearly elastic structure.

GOODYEAR MODEL [S]

This model considers the entire contact region to have the constant coefficient of friction po. 4 nonuniform pressure distribution is presumed and the adhesion limit as given by Equation (ZO), written below in terms of slip parameters,

will depend on the particular pressure distribution, qz(5), assumed. The pressure distribution may be approximated analytically or taken graphically from traction test results.

-4 technique is presented in the Goodyear paper [S] for consolidating the traction data taken over the complete range of tire operating conditions. This technique utilizes the moduli of two vectors, F and S, defined below.

7~herequirement tanaxo isn t necessary for the derivation of Equation (79). A vector S, called the slip-modulus vector, is employed to describe the slip operating conditions. Using sx and s Y as defined 8 by Equations (5) and (7) , the slip-modulus vector is

where i ar.d j are unit vectors in the positive x and y directions, respectively. The magnitude of the slip-modulus vector is S = 1SI.

The shear force distribution 0 is considered as a vector with compclnents q and q X Y

which opposes S as shown in Figure 14.

BRAKING

Figure 14. Goodyear model. Deformation and shear force distribution.

8 s and s are defined differently in [5]. X Y The shear force distribution is assumed to vary linearly with

5 in the adhesion region according to

In the sliding region, 5 > Sa, 0 is assumed to vary with the arbitrary pressure distribution q,(E), viz.,

while maintaining the direction opposing the slip-modulus vector s.

Assuming that the shear force distribution vector always opposes the slip-modulus vector allows the traction force vector F to be determined by the following integration over the contact length.

The preceding equation expresses the dependence of the traction force vector, defined as on the slip-modulus vector S given by Equation (81). This analytical dependence of F upon S involves an arbitrary expression for the vertical contact pressure distribution q,(c).

The relationship between F and S can be determined experimentally by measuring longitudinal and lateral forces over a wide range of operating conditions. For a particular tire, this data can be consolidated into a single characteristic plot of F = ;Fj1 versus

S = IS1 (Figure 15).

Traction Force F

Slip-Modulus S

Figure 15. Consolidated traction data for a hypothetical tire. The linear region in Figure 15 indicates complete adhesion with the force given by the first term of Equation (82). As sliding begins to appear (Sa < L), the plot becomes nonlinear with the influence of the second term of (82). When sliding dominates (5, = O), the limiting traction force, FS, is attained and given by the second term of Equation (82).

When enough traction data has been taken to define the relationship illustrated in Figure 15, a graphical construction can be made to determine the interaction between the longitudinal and lateral force components. Usually this is developed as a plot of Fy versus Fx at a particular slip angle as shown in Figure 16.

DRIVING

\& braking saturation

1,' S s A b

I r 1 Const ruction of tracti-on force component plot for slip angle a from consolidated data of 1:igure 15. The construction for a particular slip angle a begins by

determining the saturation slip value Ss where the limiting traction

force Fs is attained. For driving traction, Ss is laid off on the

negative x-axis and the force FS on the positive x-axis. .As the operating conditions shift from driving to braking, the vector S rotates clockwise while sweeping out the straight line (Figure 16;. The traction force vector F, always opposing S, sweeps out the desired plot according to the magnitude relationship given in Figure

15. When Ss is again reached (now in braking), the plot is terminated. A line of symmetry is found to pass through the origin and the midpoint of AB.

As the slip angle a decreases, point B describes a circular arc toward the x-axis as shown in Figure 17. Point A does not move;

DRIVING BRAKING

Figure 17. Traction force component plots at three slip angles. 49 consequently, all plots will begin at the driving saturation point C.

The traction equation (82) contains one unknown factor: the contact pressure distribution qZ(c). When sufficient experimental data is available to characterize traction behavior as in Figure 15, Equation (82), viewed as an integral equation, may be solved for the integral qZ (0. This is conveniently done by a graphical procedure outlined in [5]. The analysis of data from several tire traction testing programs indicates that the pressure distribution determined in this manner is roughly parabolic.

Closed form expressions for the traction force components Fx and F are not presented in the original publication The Y [5]. expressions for Fx and F are obtained from Equation (82) after Y the pressure distribution qz([) is determined from the analysis of experimental traction data for a particular tire.

If a uniform pressure distribution is assumed such that

the traction equations derived from the Goodyear model are identical to the traction equations of the HSR1-NBS-I model with the speed sensitivity coefficient, As, set equal to zero.

To investigate the influence of a nonuniform pressure distribution on the traction forces, the traction vector equation (82), derived from the Goodyear model, will be evaluated with the assumption of a parabolic pressure distribution, viz.,

At the adhesion limit, 5 = Ca, the contzct pressure is

The substitution of Equation (84) into Equation (80) enables the following 'a explicit equation for the adhesion fraction, -L , to be mitten.

where

is derived from the magnitude of the slip modulus vector (81).

Equations (85) and (86) show that complete adhesion = L) (5a exists only for s = s = 0, the straight ahead free-rolling X Y condition. Full sliding (Ca = O), however, takes place when the

operating conditions are such that CaS = 3uoFZ which occurs before wheel lock. This is quite different from the behavior of the HSRI-NBS-I model (see Equation (45)) where full sliding takes place only when the wheel is locked (sx = 1) although complete adhesion can exist at operating conditions other than straight ahead free-rolling.

Substituting (83) into the second term of (82), and integrating, yields the following traction force vector equation derived on the assumption of a parabolic pressure distribution.

Only two ranges, adhesion plus sliding and full sliding, are written because complete adhesion occurs only in the special case of straight ahead free-rolling (sx s = when no traction , Y 0) forces are generated. The second expression of (87) is obtained by setting ca = 0 in Equation (85).

The preceding analysis shows that the assumption of a non- uniform contact pressure distribution, such as parabolic, which vanishes at the exit point of the contact region produces the requirement for traction force generation to always be associated with a certain amount of sliding near the exit point of the contact region. Such a requirement does not exist in the HSRI models which, ~cith the assumption of uniform contact pressure, permit traction force to 5e generzted in completely adhesive contact.

The use of the slip modulus vector S, given by Equation (81), enables the components of the traction force vector F to be written as follows. These traction force component equations should be compared with

Equations (42), (43), (46), and (47) for the HSRI-NBS-I model and with Equations (64) and (65) for the HSRI-NBS-I1 model. Note that the full sliding (ca = 0) traction forces depend on the traction stiffnesses Cs and Ca. This behavior is a consequence of constraining the shear force distribution to oppose the slip modulus vector S in the sliding region.

Since the Goodyear model does not separate the tread stiffness from the carcass stiffness, the aligning moment is computed from

Equation (25) rewritten below with l/Kx = l/Ky = 0.

The shear force components, obtained from the following shear force vector equation, viz., are

(Equation (85) was used in simplifying the above expressions.) Since the contacting tread rubber is assumed to be linearly elastic (as expressed by the longitudinal and lateral stiffnesses, and k kx Y ) the displacements throughout the contact region are given by

After substituting (92) and (93) into (90) and performing the integration, the aligning moment as derived with the assumption of a parabolic pressure distribution is found to be Equation (94) shows the moment to have an implicit dependence on tire load, FZ, through the adhesion limit, ca, given by Equation (85)

Setting 5, = 0 in (94) gives the aligning moment generated in fully developed sliding (which occurs before sx = 1).

The vanishing of the adhesion region before wheel lock, a consequence of assuming a contact pressure distribution which vanishes at the contact entry and exit points, renders the

Goodyear tire model incapable of simulating locked wheel aligning moment. At a particular slip angle (s ) it is incorrect to compute Y the aligning moment at values of sx beyond those which cause the adhesion limit to vanish. A derivation and discussion of the upper bounds on sX and s imposed by the assumption of parabolic contact Y pressure is given in Appendix 111. The upper bounds are found to depend on tire load.

SAKAI MODEL [6]

Several major advances in traction force simulation are incorporated in this model. Based on an idea of W. Bergman [7], the Sakai model contains a mechanism for simulating the influence of braking and driving tractive forces (longitudinal forces) on lateral force generation. The analysis, however, differs from that L T of Bergman in that Sakai views Bergman's "effective tractive

effort" as acting along the deflected tread surface (in the

direction of motion for driving, against the direction of motion

for braking). The Bergman effective tractive effort acts in the wheel plane.

Figure 18 shows the adhesive shear forces assumed by Sakai

to be acting on a tread element deflected by braking at a slip anglc a. The Sakai effective tractive effort is the tangential

BRAKING

Figure 18. Adhesion region longitudinal and lateral forces acting on the Sakai model. The tangential tractive effort qt0

Csrce qt generated along the leflected tread surface when braking

is applied to a tire operating at a slip angle. qt = q, seca

The physical Sakai model has the tread elements attached to an elastically supported beam as shown in Figure 19.

L \ * 5 0 \ / \ K '\ 'deformed Wheel Plane Y carcass X equator

V

Figure 19. Physical Sakai model.

The elastic beam deflection in the contact region (0 -< 5 -< L) is approximated by the parabolic curve where b (length units) is the deformation constant of the elastically supported beam. The constant b, experimentally determined, depends on both the beam stiffness EI and the beam foundation modulus K . Y In the adhesion region, the tread element deformation expressions are given by Equations (13) and (14) written in terms of slip parameters by use of Equations (6) and (8).

S U = l-s 5 X

The stresses are linearly related to the deformations by the tread element stiffnesses kx and k The lateral stress, however, is Y . increased by the lateral component of the tangential q defined earlier. t

As in the Goodyear model, a parabolic contact pressure distribution is assumed according to Equation (83), repeated below. The adhesion limit, ca, is determined by equating the resultant elastic stress at this point to the maximum static friction force uoqz(ca), determined from the parabolic pressure distribution (83).

Equation (100) and the first term9 of Equation (101) are used in the left side of (103). After some algebraic manipulation, the adhesion limit is found to be

If the influence of F is neglected (rigid beam tread base), the Y adhesion fraction reduces to

'~akaineglects the last term of (101) as being small compared with the first term for the purpose of computing the adhesion limit. where CS and Ca are the braking and cornering stiffnesses defined earlier by Equations (40) and (41). Equation (105) is identical to Equation (85) derived with the Goodyear model. Complete adhesion

(5, = L) occurs only for the straight ahead, free-rolling tire.

At the adhesion limit, the static friction coefficient po immediately drops to p and the sliding shear stress shifts in direction to oppose the sliding velocity Vs. 4s shown in Figure 20,

Vcx/VS and V /Vs are the cosine and sine of the slide angle 0. cY

Figure 20. Sliding friction shear forces (braking).

-. 2)- z_;e of j6), (8), and (9), the slide angle may be expressed in terms of the slip parameters sx and s Y . (sliding region, VS = 1; ) C

The sliding friction p is assumed by Sakai to be slightly orthotropic with constant components ux and p In the consideration of this Y . treatment of sliding friction, it should be recalled that the

HSRI models consider the sliding friction p to be isotropic riith magnitude dependent on the sliding velocity VS. The Goodyear model considers the friction to be isotropic and constant throughout the contact region.

Prescribing the stress in the sliding region to have a line of action different from the stress in the adhesion region leads to a displacement discontinuity at the adhesion limit. This was recognized in the HSRI-NBS-I1 model and a transition region employed to permit gradual shift into full sliding. The Sakai model does not recognize a transition region. The displacement discontinuity present at ca may be computed as follolis where ul, v1 are dis- placements just before the adhesion limit and u2, v2 are the displacements just beyond the adhesion limit. From (98),

S X U 1 = l-s 5, X Just beyond the adhesion limit,

From Figure 20 and Equation (83),

Introducing Equations (6), (9), and (105) into the above,

The longitudinal displacement discontinuity, Au = u2 - ul, is computed by subtracting Equation (106) from Equation (107).

From (99), with nb(S) neglected,

After the adhesion limit,

From Figure 20 and Equation (83), Introducing Equations (6), (9), and (105) into the above,

The lateral displacement discontinuity, Av = v2 - v 1 ' is computed by subtracting Equation (108) from Equation (109).

The displacement discontinuity vanishes at zero slip angle - - (S = 0) if pX = uO. Since vx Y - Py - Po in most situations, the magnitude of the discontinuity depends primarily on how much the stiffness ratio

deviates from unity. Traction test results have shown the stiffness ratio to be approximately 4 for a bias tire and approximately 2 for a radial tire.

The Sakai traction forces are computed according to Equations (21) and (22) with the following shear force distributions. The discontinuity at 5 = in the longitudinal shear force 5a distribution, qx, vanishes when CS = Ca and px = po. The use of the effective tractive effort concept produces a permanent discontinuity at = in the lateral shear force distribution. 'a The beam deformation, vb(<), has been neglected in the expression for q . Y After performing the integrations and introducing the traction stiffness parameters (CS and Ca), the Sakai model traction forces may be written as follows As for the Goodyear model with a parabolic pressure distribution, only two ranges, adhesion plus sliding and full sliding, are witten because complete adhesion is possible only in the special case of straight-ahead free-rolling (sx = s = 0). Unlike the Goodyear Y model, the full sliding (Ca = 0) traction forces do not depend on the traction stiffness parameters. This is a consequence of allowing the sliding shear stress to oppose the sliding velocity instead of the direction of the "slip-modulus vector" employed in the definition of the Goodyear model. The Sakai traction force equations (111-112) should be compared with Equations (42), (43) , (46), and (47) for the HSRI-NBS-I model, Equations (64) and (65) for the HSRI-NBS-I1 model, and Equations (88) and (89) for the Goodyear model.

Since the Sakai model permits the rigid tread base to translate laterally on an elastic foundation of modulus K the aligning Y' moment is computed according to Equation (25) as rewritten below with l/Kx = 0. The shear stress distributions, qx and qy, are given by Equations (110). For the express purpose of evaluating Equation (113), the following simplified set of displacement distributions, u and v, are assumed which ignore the longitudinal displacement u entirely and consider the lateral displacement v in the sliding region to decrease linearly to zero at the contact exit point.

Figure 21 illustrates the tread element deformation assumed for the moment computation. The linearly decreasing displacement in the sliding region is a more realistic approximation than the uniform sliding region displacement assumed by the HSRI-NBS-I model (see Figure 8). Note also that displacement continuity is maintained for the moment computation although the shear stresses, qx and qv, still contain the discontinuity across which the traction forces were computed. Figure 21. Displacements assumed by the Sakai model for the computation of aligning moment.

Denoting the adhesion region contribution to the aligning moment by bIT and taking the shear force and displacement distri- butions from (110) and (114), the first integral of (113) is evaluated as follows.

After performing the integration and introducing the traction stiffnesses C and Ca, S Denoting the sliding region contribution to the aligning moment by >I", the second integral of (113) is evaluated as follows.

After performing the integration,

The aligning moment equation (113) is now where b2' and M" are given by Equations (115) and (116). The complete expression for the Sakai aligning moment is

where the traction forces, Fx and F are given by Equations (111) Y' and (112).

Setting Ea = 0 in Equation (117) yields the aligning moment generated by the Sakai model in fully developed sliding.

Favorable experience gained during the study of the Goodvear and Sakai tire models, which assume a parabolic contact pressure distribution, has led to the incorporation of a parabolic pressure distribution, 9, , in a rederivation of the force and moment equations of the IISRI-NBS-I1 model. This modification, which substantially changes the traction characteristics obtained from the HSRI-NBS-I1 model with uniform contact pressure, is the basis of the HSRI-NBS-I11 tire traction model.

The parabolic contact pressure distribution is defined to vanish at the entry (5 = 0) and exit (5 = L) points of the contact region. The parabolic expression, Equation (83) used in analysis of the Goodyear model, is

where

is the tire load.

The adhesion limit is obtained by substituting Equation (83) evaluated at 5 = 5,, into Equation (60). After rearrangement, the result obtained is the adhesion fraction previously derived for the Sakai model

with Cs and Ca the braking and cornering stiffnesses defined by

Equations (40) and (41). The limit of the transition region is obtained by substituting

Equation (83), evaluated at 5 = Cs, into Equation (59). After rearrangement, the result is written as the transition limit fraction

It is evident from Equation (105) that complete adhesion

(5, = L) will occur only for straight-ahead (s = O), free- Y rolling (sx = 0) tire operation. As Equation (119) shows that

< L for all conditions other than straight-ahead free-rolling, s and 5, 5 Es, the HSRI-NBS-I11 model will always exhibit a certain amount of sliding in the contact region.

The traction forces, Fx and F Y' are obtained by using the parabolic pressure distribution in evaluating the terms of

Equations (64) and (65). The adhesion region terms, Fxa and

F are unchanged as they do not depend on the tire load, FZ. ya' In the transition region, the shear stress distribution is assumed to be parabolic in accordance with the vertical contact pressure. It is therefore necessary to prescribe parabolic functions for the displacements, ut (5) and vt (S) in the transition region. a a, I= rl cd C, P 0

d a,. k n cd w I .. 4 C, u h 7 F4 A0 a I F= cd cb w V C, X L.. V)

a,E I t'

n a, w U I k V) 0 w w V F: 0 cd .ti LJJ' M cd a, > I k 94 5 d 4 It' C, .d II V) F: C, cd > k C, a, A E- - S 2 = -C (>) Ya al-sX Referring to Equations (105) and (119), it is seen that

the adhesion and transition regions vanish before wheel lock

(sX = 1). If the tire operating conditions are such that

5, = 0 but 5, > 0, the resulting traction forces, from Equations

are seen to be equivalent to the traction force expressions for full sliding contact (5, = tS = 0). Equations (124) should be compared with the analogous Equations (69) for the HSRI-NBS-I1 model. The longitudinal slip parameter, sx, appears in

Equations (124) because full sliding occurs before wheel lock.

The aligning moment, MZ, is obtained by using the parabolic pressure distribution in evaluating the terms of Equation (71).

The adhesion region term, ?IZa, being independent of tire load, is unchanged.

The transition region term, ?.IZt, is found by a rather lengthy integration

with u = ut and v = vt where ut, vt are given by Equations (120)

'a - La) + 2 cr"1 )(:.- -

This expression should be compared with Equation (76) derived for the HSRI-NBS-I1 model which employed the assumption of uniform contact pressure. The tire characterizing data required to operate the five tire models described in this document are gathered by laboratory and over-the-road tests of the actual to be represented by the models. It is frequently necessarJ- to adjust certain of the measured tire data in order to obtain an improved simulation of tire traction characteristics. This practice, made necessary by the gross approximations inherent in all tire models, is common in the simulation of complex phenomena other than tire traction. The measurement techniques and data processing procedures used to obtain input data for the various tire models are discussed in this chapter.

Since most, if not all, of the tire data required for operation of the tire traction models is significantly dependent on inflation pressure, the data gathering procedures must be per- formed with the actual tire at the inflation pressure for ~~hich traction response simulation is desired.

Figure 22 arranges the collection of model input data required to characterize an actual tire according to the type of test

(standing or rolling) required. The acquisition of each piece of tire characterizing data listed in Figure 22 will be described in the following sections. Data from an FR70-14 radial tire, whose footprint is shown in Figure 23, is used to illustrate the acquisition procedures. L contact patch length

Standing Tests Kx longitudinal carcass spring rate K lateral carcass spring rate Y

CS longitudinal traction stiffness C lateral traction stiffness C1 Rolling Tests limiting coefficient of static 'O 'O friction speed sensitivity parameter As XI orthotropic sliding friction pY coefficients

Figure 22. Tire and tire-road characterizing data for operation of tire traction models.

STANDING TIRE TESTS

The contact patch length and carcass spring rates are measured on the standing tire, statically loaded the operating value

Fz. The HSRI Flat Bed Tire Tester [8] is used to obtain these measurements.

CONTACT PATCH LENGTH L. The patch length is measured on the

+L~re . footgrint obtained by inking the tread with a stamp pad and deflecting the inked tread against a heavy sheet of graph paper. Figure 23 reproduces a print obtained in this manner with a Figure 23. Inked tread footprint of a standing radial tire FR70-14 inflated to 24 psi and statically loaded at 1000 lb. radial tire under a vertical load FZ = 1000 lb. As the contact perimeter generally deviates from the rectangular one assumed by tire models, a mean value is estimated (by eye) such that the rectangular area corresponds to the actual area.

1:igure 24. Variation uT contact klatch lcngt11 with vcrticul load for a radial tire FR73-14 inflated to 24 psi. 8 0 LONGITUDINAL CARCASS SPRING RATE Kx. The load-deflection measurements leading to the longitudinal spring rate are made with rhe wheel plane in the direction of flat bed travel. The deflected tire is locked against the flat bed table which is manually moved

in increments of .1 inch. Longitudinal force readings are taken at each displacement until the tire begins to slide. The onset of tire sliding is evident in the representative data for a radial tire shown in Figure 25. The longitudinal carcass spring rate is the

x-X-900 lb.

Longitudinal ------1600 lb. Force Fx (lb) p = 24 psi 400 t

? .1 . L .3 .4 .5 Table Travel (in)

Figure 25. Longitudinal force (F,) versus travel of flat bed table supporting a radial tire at the indicated vertical loads. slope of the linear portion of the longitudinal load-deflection plot. As seen in Figure 25, the slope is essentially constant for

the 900, 1100, and 1600 lb. vertical loads. The approximate value of Kx = 1000 lb/in is obtained at these loads.

K LATERAL CARCASS SPRING RATE Y . The lateral spring rate is obtained from load-deflection measurements made with the wheel plane perpendicular to the direction of flat bed travel. Lateral force measurements are made as the flat bed table is moved in small

increments until the tire begins to slide. The lateral carcass spring rate is the slope of the linear portion of'the resulting lateral load-deflection plot. As seen in Figure 26, tire vertical load has little influence on the lateral spring rate of a radial tire. The value of K = 500 lb/in is obtained from the data shown Y in Figure 26.

COMMENT ON CARCASS SPRING RATES. Since the hollow carcass structure is considerably more compliant than the solid tread structure (even with grooves), the lateral and longitudinal spring rates measured by the procedures described above are essentially those of the tire carcass. This argument would be supported by an experiment (not yet performed) whereby the carcass is rigidized in the deflected position and the procedures repeated to obtain f!?e data shown in Figures 25 and 26. Substantially higher slopes \could result for the tread spring rates Kx and K *. Recognition Y that the carcass-tread combination behaves elastically like springs

*Not to be confused with kx and k which are spring constants of the hypothetical tread elements uxed to derive various models of traction response characteristics. 24 psi

-0-8- 700 lb. -XX900 lb. A41100 lb. 001600lb.

Table Travel (in)

Figure 26. Lateral force (F ) versus travel of flat bed table supporting a radyal tire at the indicated vertical loads. in series explains how the much softer carcass spring Kx dominates ---%a- K x, Y Kx ,Y the data from these experiments which really measure the effective spring rate of the carcass-tread combination.

ROLLING TIRE TESTS

LONGITUDINAL TR4CTION STIFFNESS CS. The longitudinal traction stiffness is defined by Equation (38), repeated below.

Graphically, this parameter is the slope at the origin of the longitudinal force (Fx) versus longitudinal slip (sx) data measured Figure 27 shows flat bed Fx versus s in straight-ahead rolling. X data for the FR70-14 radial tire operated at several loads. The slope through the origin of this data is seen to be nearly inde-

en dent of tire load. The longitudinal traction stiffness for this tire, derived from the data shown in Figure 27, is approximated by

C = 20,000 lb/unit slip S Ib.

i .2 .4 .6 .8 1.0

i Longitudinal Slip (sx)

Figure 27. Longitudinal force (Fx) versus longitudinal slip (s ) developed by a radial tire FR70-14 at the inaicated tire loads and 24 psi. LATERAL TRACTION STIFFNESS C,. The lateral traction stiffness is defined by Equation (39), repeated below.

Graphically, this parameter is the slope at the origin of the lateral force (FY ) versus slip angle (a) data measured in free rolling. Figure 28 shows a carpet plot of flat bed F versus a Y and tire load (FZ) data for the FR70-14 radial tire. It is seen that the slope at the origin of each of the constant load curves are nearly equal to the slope at the origin of the FZ = 1100 lb curve which is found to be

COMMENT ON TRACTION STIFFNESSES. The traction stiffnesses,

Cs and Ca are measures of the traction force generating ability of a tire operated at small values of sx and s (a). Although Y strictly valid only for traction forces which respond linearly to the operating variables sx and a, i.e.,

and the range of application is extended by the structure of the semi-empirical tire model. Thus the traction stiffnesses are employed in equations of the form Figure 28. Lateral force (F ) versus slip angle and vertical load. Radial tire ~~70Y14at 24 psi.

8 7 which simulate the nonlinear response of F to sx and the influence X of sx on the generation of lateral force F . The simulation is Y better at small values of sx and s for which the rolling tire Y contact is mainly adhesive.

If the traction forces could be generated with completely adhesive contact, it would follow that Cs and CU would be inde- pendent of tire-road friction properties and be measures solely of the influence of tire structure on traction force generation. Over-the-road experimental evidence, however, indicates that the traction stiffnesses do depend on road surface and contact contamination as well as tire load and velocity. Such dependencies are produced by a certain amount of sliding in the contact region.

Observing that wer-the-road traction stiffnesses are generally somewhat less than flat bed traction stiffnesses, the values of

~ihic;~are 20% less than the flat bed stiffnesses found for the FR70-14 radial tire are taken as tire characterizing data for model comparison purposes. TIRE-ROAD FRICTION PARAMETERS AS, ux, p The study of ", Y . tire-road friction characteristics has not progressed to the stage where it is possible to define a procedure for determining the 10 values of the friction characterizing parameters appearing in Equation (30)' repeated below.

The current practice is to set the limiting static friction coefficient, lio at some nominal value which will produce realistic peak traction forces Fx and F The speed sensitivity factor, As, is then adjusted Y . for optimum simulation of traction data at higher values of sx and s (simulation when the sliding region becomes significant). Y As both po and As influence the location of the adhesion limit, and consequently the magnitude of peak and F some 'a1 Fx Y' iteration (a new adjustment of po and then of may be necessary to set both parameters for optimum simulation of the complete traction force curves.

'O~he optimum form of the friction characterizing function (30) has not yet been determined. As explained in Reference [9], the assumption of a linear relationship (30) between friction and slip speed is largely pragmatic; being made in the absence of experi- mental data which ~~ouldmore closely define this very important relationship. It is believed that the linear approximation agrees sufficiently well with the qualitative aspects of experimental findings to justify its current adoption. The orthotropic sliding friction coefficients, px and py,

employed by the Sakai model, reflect speed sensitivity by taking a slightly lower value than the limiting coefficient of static

friction po.

The following values of po, AS, pX and p Y were used in producing the model comparisons discussed in the next chapter.

= 1.0

As = 0.0035

- = 0.9 (isotropic sliding friction) lix - Py MODEL RESPONSE COMPARISONS

The tire model responses for the following comparisons were all calculated with FR70-14 radial tire characterizing data derived by the procedures discussed in the preceding chapter. The following model input data values were used.

L = 7.5 inches (contact length)

= 1000 lb/in Kx (carcass spring rates) K = 500 lb/in Y

C = 16,000 lb/unit slip S (traction stiffnesses) C a = 8,000 lb/radian

= 1.0 (static friction coefficient) Po

A = 0.0035 (speed sensitivity factor) S

- = 0,9 (isotropic sliding friction) x P~

The tire load was set at FZ = 1000 lb and the traveling velocity at V = 25 ft/sec.

The tire models were operated over a range of sx and s values Y covering driving and braking at slip angles varying from zero to 16 degrees. The computer-drawn plots in the following figures illustrate traction force and moment response as a continuous function of longitudinal slip, sx. Each curve is calculated for the indicated slip angle a (s = tana). Y The MSRI tire models which assume uniform contact pressure do not show loss of adhesion until the wheel is locked (sx = 1) or the slip angle is 90 degrees. The Goodyear and Sakai models, which assume parabolic contact pressure, show loss of adhesion at rather low values of longitudinal slip. This behavior is analyzed in Appendix I11 where upper bounds are derived for the slip parameter values which produce a finite adhesion region. With the assumption of a contact pressure distribution which vanishes at the entry and exit points, the upper bound on sx, i.e., the value of sx when adhesion is lost, depends on the slip angle a (s ). Y For the parabolic contact pressure distribution, the upper bound on s is calculated with Equation (111-16) derived in Appendix 111. X Table 1 lists the upper bounds on sx calculated for the FR70-14 radial tire characterizing data used in the model response comparisons. The maximum slip angle at which this tire could be

TABLE 1

Slip Lateral Slip Upper Angle Parameter Bound aO s =tana s Y X

- -- - operated with retention of an adhesion region is approximately a = 20 degrees. The dashed lines on the following Goodyear and Sakai traction force and moment plots connect loss of adhesion points. The model response plots have been drawn for higher values of sx although it is emphasized that the models have limited capability for simulating full sliding behavior as a function of longitudinal slip, sx. To cite an example, the Goodyear traction force plots (Figs. 292,

30c) appear to show a smooth transition from adhesion to full sliding, however, the Goodyear moment response (Fig. 33c) becomes unstable when loss of adhesion occurs.

TRACTION FORCE COMPARISONS

LONGITUDINAL TRACTION FORCE. Figure 29 presents the longi- tudinal traction force response of four models operated at five slip angles. The HSRI-NBS-I and I1 models assume a uniform contact pressure and thus carry the simulation out to the locked wheel condition (sx = 1). The assumption of a tire-road friction coefficient which decreases with increasing slip speed, Equation

(30), permits the HSRI-NBS-I and I1 models to show decreasing longitudinal traction force, Fx, after the peak is reached. This behavior is evident in the force curves at 0, 4, and 8 degrees slip angle (Fig. 29a,b). The decrease in Fx at lower values of the slip angle is confirmed by experimental evidence [lOll'. The Goodyear and Sakai models, which assume parabolic pressure, appear to show a slight peak in Fx at the zero degree slip angle (Fig. 29c, d) before adhesion is lost.

ll~hequantitative matching of model response to the referenced experimental data [lo] has not yet been attempted. A quantitative validation study is planned. * .2 3 't -6 ~8 I. Longitudinal Slip sx Longitudinal Slip sx

-8

0 6

Loss of adhesion

Longitudinal Slip sx Longitudinal Slip sx

I:igur-e 29. Comparison of longitudinal force (F /F ) versus longitudinal slip (s ) rcsponse of feu$ tire traction rnodcls operated at tfie indicated slip angles. Radial tire I:R70-14 data input. Figure 30 compares the straight-ahead longitudinal traction force response of the five models analyzed in this document. The transition region apparently has little effect on straight-ahead longitudinal force generation as the HSRI-NBS-I and I1 models produce nearly the same curve. The HSRI models which assume a frictioncoefficient decreasing with slip speed, show Fx decreasing slightly as sx increases after the peak while the Goodyear and Sakai models, which assume constant friction, show flat responses after the peak.

LATERAL TRACTION FORCE. Figure 31 presents the lateral traction force versus longitudinal slip response of four models operated at four slip agles. The lateral traction force curves from the HSRI-NBS-I and 11, and the Goodyear models (Fig. 31a, by c) all show peak lateral force at nearly zero longitudinal slip. The Sakai model (Fig, 31d) shows the lateral force peaks at noticeably higher values of longitudinal slip (s). The lateral force response of the Sakai model is qualitatively closer to experimental data which generally show peak lateral force tending to appear at smaller values of sx as slip angle increases. The improved lateral force response of the Sakai model is attributed to the unique mechanism which this model contains for simulating the interaction of longitudinal force with the development of lateral force in the adhesion region. Conji tdind

Force (ib)

Figure 30. Comparison of the straight-ahead longitudinal force response of the five models analyzed in this document. (a) HSRI-NBS-I

Longitudinal Slip sx Longitudinal Slip sx

ssof adhesion

I\ \ \ (dl Sakai

Longitudinal Slip sx Longitudinal Slip sx

Figure 31. Comparison of lateral force (F /FZ) versus longitudinal slip (s ) response of four tirg traction models operated at the fndicated slip angles. Radial tire FR70-14 data input. The model comparisons of free-rolling lateral force response,

Figure 32, show the HSRI-NBS-I11 model producing the same curve as

the Goodyear model and nearly the same curve (at smaller slip angles) as the Sakai model. These models assume a parabolic contact

pressure distribution. The HSRI-NBS-I and I1 models, which assume

a uniform contact pressure distribution, produce a different curve.

The adhesion region, which decreases with slip angle, is present

at a = 16 degrees and contributed to the lateral force curves

shown in Figure 32.

Figures 33 and 34 compare the simulation of the interaction

of longitudinal force with lateral force. The HSRI-NBS-I and I1 models (Fig. 33) produce nearly identical plots. These HSRI models

differ mainly in the treatment of the transition from adhesion to

full sliding. Little traction force is apparently generated in

the transition region for the operating conditions which produced

these plots. Substantial differences are seen in the plots from

the Goodyear and Sakai models. These differences are again attributed to the Fx-F interaction mechanism incorporated in the Y Sakai model. The comparison of the Goodyear plot, Figure 34a, with

the HSRI-NBS-I plot, Figure 33a, indicates the effect of parabolic

contact pressure vis 2 vis the effect of uniform contact pressure. Figure 32. Comparison of the free-rolling lateral force response of the five models analyzed in this document. (a) HSRI-NBS- I

'I . (b) HSRI-NBS-I1

Figure 33. The interaction of longitudinal force (Fx/FZ) with lateral force (F /F ) generated at the indicated slip angles. ~a8iaftire FR70-14 data input to two tire traction models which assume uniform contact pressure. Figure 34. The interaction of longitudinal force (F /F ) with lateral force (F /F ) generated at the ifidigated slip angles. ~a8iaftire FR70-14 data input to tire traction models which assume a parabolic distribution of contact pressure. Figure 34 (c) . HSRI-NBS- I11 The interaction of longitudinal force (Fx/FZ) with lateral force (F /FZ) generated at the indicated slip angles. Radial Y tire FR70-14 data input to the HSRI-NBS-I11 tire traction model which assumes a parabolic distribution of contact pressure. ALIGNING MOMENT COMPARISONS

A more stringent test (than traction force response) of tire model realism is the capability for simulating aligning moment.

Examination of Figure 35, comparing the aligning moment response of three tire models, reveals major differences in the simulations,

Whereas the traction force simulations comyared in ligu~es29 and

31 are of essentially the same form and magnitude, the magnitude as well as the form of the aligning moment response plots show considerable variation. The Goodyear aligning moment response

(Fig. 35c) has very low magnitude and is unstable after loss of adhesion. The Goodyear moment response when adhesion is present is shown on an expanded scale in Figure 35d.

Figure 36, comparing the free-rolling aligning moment response of the four models for which aligning moment equations were derived, shows the variation between the models. The exceedingly low amplitude of the Goodyear moment response may be attributed to lack of carcass flexibility. The other three models plotted utilize the carcass spring rates Kx and K Y . Figure 37 illustrates the influence of carcass flexibility on aligning moment simulation. It appears that carcass flexiblity, described by the spring rates Kx and K is essential for the Y' magnitude of the aligning moment simulation to approach a realistic value. The lack of carcass flexibility in the Goodyear model partially explains the low magnitude of the aligning moment response.

The carcass spring rates Kx and K inasmuch as they are associated Y' with uniform carcass translations,do not influence the generation of traction force (Fx and F ). Y - I. , Mz m in-lb

(a) HSRI-NBS-I1

-- I , 82 , 'f ,6 1 f I, Longitudinal Slip sx

M in-lb

(d) Goodyear (expanded scale) 12

08 , udinal Slip sx

Figure 35. Comparison of aligning momend (MZ) versus longitudinal slip Isx) response of three tire traction models operated at the indicated slip angles. Radial tire FR70-14 data input. Aligning Moment (in-lb)

Slip Angle (deg)

Figure 36. Comparison of the free-rolling aligning moment response from four traction models. Figure 37. Comparison of the interaction of longitudinal lorcc 1 with aligning moment (M ) generated at the indicated slip angles using HSRI-RBS-11 model with and w-ithout a tread base sprlng foundation. REFERENCES

"Vehicle Ilynamics Terminology," SAE Recommended Practice J670c, SAE Handbook Supplement J670c, January 1973. Clark, S.K., ed., Mechanics of Pneumatic Tires, NBS Vonograph 122, November 1971. Dugoff, H., et al., "An Analysis of Tire Traction Properties and Their Influence on Vehicle Dynamic Performance," 1970 Inter. Auto. Safety Compendium, SAE, pp. 341-366. SAE Paper No. 700377. Fancher, P.S., et al., Tire Traction Grading Procedures as Derived from the Maneuvering Characteristics of a Tire-Vehicle System (Volume 11), Final Report, NBS Contract No. 1-35715, mySafety Research Institute, University of hlichi~an,-. . Ann Arbor, ~une13, 1972. Livingston, D.I., and Brown, J.E., "Physics of the Slipping Wheel. 11. Slip Under Both Tractive and Lateral Forces." Rubber chemistEy and Technology, Vol. 43, No. 2, 1970 ' (pp. 244-261). Sakai, H., "Theoretical Study of the Effect of Tractive and Braking Forces on Cornering Characteristics of Tires," Safety Research Tour Paper No. 4, Oct-Nov. 1969, Stability and Control Committee, Society of Automotive Engineers of Japan. Bergman, W., "Theoretical Prediction of the Effect of Traction on ," SAE Transactions, Vol. 69, 1961 (pp. 614-640). Tielking, J.T., et al., "Mechanical Properties of Truck Tires," SAE Paper No. 730138. Dugoff, H., et al., Tire Performance Characteristics Affecting Vehicle Response to Steering and Braking Control Inputs, Final Report, NBS Contract No. CST-460, Highway Safety Research Institute, University of Michigan, Ann Arbor, August 1969. Tielking, J.T., Construction and Profile Study, Part I: Tire Traction Data Measured by the HSRI Mobile Tire Tester, HSRI Project 329180, Tire Traction Characteristics Affecting Vehicle Performance," Interim Document 5, March 1973. u SYMBOLS AND TERMINOLOGY speed sensitivity factor braking/driving traction stiffness cornering traction stiffness aligning traction stiffness tread base bending stiffness

Traction force vector

traction force saturation magnitude longitudinal tire traction force

F xa adhesion region contribution Fxt transition region contribution F sliding region contribution XS lateral tire traction force

F adhesion region contribution Ya F transition region contribution Yt F sliding region contribution YS tire load unit vectors in x and y directions longitudinal and lateral carcass stiffnesses longitudinal and lateral tread element stiffnesses contact patch length (standing tire) longitudinal and latcral traction force ofiscts aligning moment

Mza adhesion region contribution transition region contribution MZ t MZs sliding region contribution magnitude of shear force distribution vector tangential tractive force (Sakai) components of the shear force distribution vector contact pressure distribution effective rolling radius slip modulus vector (Goodyear)

slip modulus magnitude at traction force saturation longitudinal and lateral slip parameters time, transition region length longitudinal and lateral tread element displacements uniform longitudinal and lateral carcass translations tread element displacements at the adhesion limit (a tread element displacements at the transition limit tS nonuniform displacements within the transition region traveling velocity vector components of the traveling velocity vector slip velocity vector components of the slip velocity vector rolling velocity sliding velocity vector contact patch width (standing tire) tire coordinates slip angle inclination angle slide angle parameter used in defining the transition region sliding friction coefficient limiting coefficient of static friction orthotropic sliding friction coefficients contact coordinates limit of the adhesion region limit of the transition region shear force distribution vector rotational velocity of the wheel about the axle APPENDIX I MODEL KESUMES

The following five models were selected for analysis in this document because of their ability to simulate tire traction forces and moment in response to both lateral and longitudinal slip.*

The salient features of each model are summarized in the fo?lo\iiilg resumes.

MODEL RESUME HSRI-NBS-I [3] Elastic tread blocks on rigid wheel, uniform contact pressure, uniform deformation in sliding region, tire-road friction decreasing linearly with slip speed. Aligning moment not simulated. HSRI -NBS-I I [4] Elastic tread blocks on foundation allowed to translate uniformly, finite transition between adhesion and fully developed sliding, uniform contact pressure, distinction between static and dynamic friction which decreases linearly with slip speed. Goodyear [5] Elastic tread blocks on rigid wheel, parabolic or experimentally determined contact pressure, deformation in sliding region decreases with shear force, constant friction. Deformation discontinuity avoided by assuming sliding shear force to act in same direction as shear force in the adhesion region. Sakai [6] Elastic tread blocks on flexible elastically- supported beam carcass (subsequently reduced to rigid beam with uniform translation) with an artificial mechanism connecting longitudinal stiffness with lateral stiffness (but not vice-versa), parabolic contact pressure, distinction between static and sliding friction which is considered to be orthotropic. Pre- scribed stress in sliding region produces a displacement discontinuity for unequal longi- tudinal and lateral traction stiffnesses. Traction forces and moment computed by integrating

*The "classical" string and beam models treat the tire as free- rolling and are thus excluded. across a stress discontinuity which is more severe for bias tires than for radial tires. Parabolic contact pressure, otherwise identical to HSRI-NBS-I1 model. APPENDIX 11 SUMMARY OF FORMULAS

The adhesion limit equations and the traction force and moment equations associated with the five models are collected in this appendix. The digital computer programs listed in Appendix IV evaluate the force and moment equations as written here in terms of the slip parameters sx and s Y'

HSRI-NBS-I [3]

Adhesion Limit

where

Traction Modes

> L complete adhesion 'a -

0 < 5, < L adhesion and sliding

5, = 0 complete sliding (only at wheel lock) Traction Forces HSRI-NBS-I1 [4]

Adhesion Limit

Transition Limit

where

Traction Modes -

'a 'a -> L complete adhesion

La < 5, -> L adhesion and transition adhesion and transition and sliding 'a < 5, < L

's -< 5, < L adhesion and sliding

5, = 0 complete sliding (only at wheel lock)

Traction Forces where

S 's F = -flz x (1 - XS (In- X Y

Aligning Eloment

where Note

Fxa3 Fyay M za are terms contributed by the adhesion region which exists when 0 < 5 < L. a -

Fxt' F yt' MZt are terms contributed by the transition region which exists when 0 <

F F M are terms contributed by the sliding region XS' ys' zs which exists when 5,) 5, < L. GOODYEAR MODEL [5]

Adhesion Limit (for parabolic contact pressure)

Traction Modes

O

complete sliding (occurs before wheel lock) 'a = 0

Traction Forces Aligning Moment SAKAI MODEL [6]

Adhesion Limit

Traction Modes

adhesion and sliding

complete sliding (occurs before wheel lock)

Traction Forces Aligning Moment

L - 5 [3(c, + Cssx) - X

L

M = z X Y - FxFy/Ky 0

Transition Limit

where

.P = po(l - A&] ; vs - x Y IVI cosa

Traction Modes

'a ' 's < L adhesion and transition and sliding

cs 1 'a < L adhesion and sliding

'a = 0 complete sliding (occurs before wheel lock)

Traction Forces where

s 5a F = -C -iY- (r) Ya al-sX

s 'a 's 'a 'a F ; - [LC -iY- (3 - 2r-r)r/(l ~t 3 al-sx

Aliening Moment

where d F M are terms contributed by the adhesion region -xa' ya' za which exists when 0 < 5, < I.,.

are terms contributed by the transition region Fxt' Fyt' MZt which exists when 0 < Ea < 5, < L.

F F M are terms contributed by the sliding region xs' ys9 zs which always exists when a parabolic pressure distribution

is presumed. 124 It is interesting to note that all of the expressions summarized in this appendix can be normalized (dimensionless) with respect to FZ and L by the following substitutions.

Therefore,

This procedure is particularly useful in computer implementation of the models as explained in Appendix IV. APPENDIX 111 LOCI OF ADHESION LIMIT POINTS

The adhesion limit point, 5 = Ea, depends upon the contact pressure distribution qZ([) as well as the slip parameters sx and s . The shape of the contact pressure distribution produces certain Y values (upper bounds) of the slip parameters which initiate full sliding

w operation of the linear tire models* discussed in this document. The upper bounds on the slip parameters are determined by considering the loci of the adhesion limit points for the pressure distribution function assumed. Two contact pressure distributions, uniform and parabolic, will be analyzed in this appendix.

UNIFORhI CONTACT PRESSURE q, = F~/HL

Equation (20), solved for the adhesion limit in terms of slip parameters and traction stiffnesses, becomes

The tread element deformation, ua and va, at the adhesion limit, are given by Equations (18) and (19) written in terms of slip parameters.

*The term 'linear tire model' is applied to those models which consider contact shear stress as a linear function of shear deformation. 176 Equation (111-1) may be solved for sY and used to eliminate s Y and Ca. from (111-3). The result expresses va in terms of s X

The coordinates, ua and va, of the adhesion limit point, A (Fig.

111-I), have now been written independent of s The locus of the Y . adhesion limit points, as the adhesion limit moves back from the contact entry point, is given by

Figure 111-1. Coordinates of the adhesion limit point A . For analyzing the locus of points A, it is convenient to define a new independent variable 5 such that

The locus of adhesion limit points, for uniform contact pressure, may now be written as

The uniform pressure locus (111-6) is found to be elliptical with lateral semi-axis independent of sx. The elliptical locus, which occurs for s < 1, is shown as a dashed line in Figure 111-2. X

Figure 111-2. Loci of adhesion limit points (A) for uniform contact pressure. 128 The adhesion limit for a free-rolling tire with uniform contact pressure is at

and the locus of adhesion limit points is the horizontal straight line

shown in Figures 111-2 and 111-3.

Figure 111-3. Locus of adhesion limit points (A) for a free-rolling tire with uniform contact pressure. The preceding study of adhesion limit point loci reveals the following slip parameter ranges producing an adhesion region in a linear tire model with the assumption of uniform contact pressure.

Since Equation (111-1) shows the adhesion limit 5, to vanish only for sx = 1, the adhesion operating range of sx is

Figure 111-2 shows that for all sx f 1, the adhesion limit will vanish only for cl = 90" (5 = a). The adhesion operating range Y of s is Y

PARABOL IC CONTACT PRESSURE

For a parabolic contact pressure distribution evaluated at

5 = 5 a' Equation (20), solved for the adhesion limit in terms of slip parameters and traction stiffnesses, becomes

Solving Equation (111-9) for sY and using the result in (111-3) allows va to be written in terms of sx and 5,. The coordinates of the adhesion limit point, A (Fig. 111-I), are u given by (111-2) and va given by (111-10) above. These coordinates a are independent of s and allow the limit point locus to be Y expressed as an explicit function of Sa (or 5). The locus of adhesion limit points, for parabolic contact pressure, is

where 5 is the independent variable defined by (111-5). The parabolic pressure locus (111-11) is found to be lemniscatic with finite slope at the origin. The analysis of (111-11) is facilitated by rewriting it in the following form.

For a particular value of sx, Equation (111-12) has the functional form

where A, B, and C are constants depending on sx. Nonzero adhesion limits exist when B > C/A, for which Equation (111-13) exhibits the two curves whose essential features are shown in Figure 111-4. Figure 111-4. Sketch of adhesion limit locus equation (111-13).

The adhesion limit locus is confined to the upper half of the lemniscatic loop in the region 0 -< 5 -< (B - c/A), Recognizing that

the adhesion limit locus exists only for (B - C/A) > 0 determines the upper bound for sx at The adhesion limit vanishes for straight-ahead braking when sx attains the value given by Equation (111-14). For braking at a slip angle, the adhesion limit vanishes somewhat before the sx value given by (111-14).

The adhesion limit locus for sX below the upper bound is shown in Figure 111-5. The lemniscatic nature of the locus is retained as sx drops to zero for the free-rolling tire. At sx = 0, the locus becomes a parabola crossing the axis at the contact exit

L point (5 = -).1-sx

Figure 111-5. Locus of adhesion limit points for parabolic contact pressure. As the slip angle a is increased from zero, the adhesion point A moves forward in the contact patch until it reaches the contact entry point at Ea = < = 0. As seen in Figure 111-5, the upper bound for the slip angle (and the parameter s occurs at the finite Y ) slope of the adhesion limit locus passing through the origin. The first derivative of Equation (111-13), evaluated at the origin, is

Introducing the constants A, B, and C from (111-12) yields the upper bound to the slip angle a as the limit slope sY .

Solving Equation (111-15) for sx gives the upper bound to s when a slip angle is present. X

A slightly lower limiting value for sx results for nonzero s Y . When s = 0, Equation (111-16) reduces to Equation (111-14). Y The adhesion limit for a free-rolling tire with parabolic contact pressure is obtained by setting sx = 0 in Equation (111-9). As predicted by the above and Equation (111-IS), the free-rolling adhesion limit vanishes when

Setting sx = 0 in Equation (111-11) results in the parabolic locus of adhesion limit points

shown in Figure 111-6. The locus is proportional to the parabolic contact pressure.

Figure 111-6. Locus of adhesion limit points for a free-rolling tire with parabolic contact pressure. As the slip angle increases, the sliding region contact points will follow the adhesion limit locus. This is a special case.

In general, the sliding contact points will not follow the adhesion limit locus which terminates inside the contact region (except for s = 0). X

The preceding analysis has determined the following slip parameter ranges producing an adhesion region in a linear tire model with the assumption of prabolic contact pressure.

For straight-ahead braking, the upper bound on sx is given by

Equation (111-14) and the adhesion operating range of sx is

O), In the presence of a slip angle (sY > the upper bound on sx is reduced to the value given by Equation (111-16).

In free-rolling cornering, the upper bound on s Y is given by Equation (111-17) and the adhesion operating range of s Y is

In the presence of braking (sx > O), the upper bound on s Y is reduced to the value given by Zquation (111-15). APPENDIX IV

I (; ITAL COMPIJTlill I'I1OGILAMS

The digital computer programs described and listed in this appendix are written in FORTRAN IV for execution on the HSRI

PDP 11/45 computer with 64K (bytes) of core memory. The traction response plots were drawn by a Calcomp 565 digital plotter controlled by the PDP 11/45.

TI RE MODEL SUBROUTINES

The five tire models, whose descriptive equations are summarized in Appendix 11, have been programmed as FORTRAN sub- routines. The programming has employed the normalization scheme described at the end of Appendix 11. Thus, the computed traction forces FX and FY should be multiplied by the tire load FZ to obtain the dimensional values. The computed aligning moment 1)IZ should be multiplied by FZ*L to obtain the dimensional value,

The tire model subroutines are identified by a five-character name and a model code number as listed in Table 2. b

TABLE 2

TIRE MODEL SUBROUTINE NAMES AND CALLING CODE NUblBERS

Sub routine Tire Calling Name Flo de 1 Code

NMH S1 HSRI-NBS-I

NMHS 2 HSRI-NBS-I1

NMHS 3 HSRI-NBS-I11 NMSKl SAKA I

NMGDR GOODYEAR The tire model subroutines may be called from either of

two main programs, W1DGT1 and NMDGT2, developed to exercise the

models.

MA I N P ROG RAMS

Two main programs were developed for the purposes of

obtaining the comprehensive traction response of a specific tire model (NMDGT1) and to compare the traction response of all

five tire models in either free-rolling or straight-ahead

operation (NMDGT2).

NMDGT1. This main program calls a specific tire model

identified by the calling code input datum IMODE. The value of

the input datum ISWl selects the slip variable (a or sx) to be

swept at discrete values of the nonswept variable (sx or a)

assigned by a DATA initialization statement. The nonswept

variable is called the path variable. Subroutine PATHl is

called by NElDGTl if an a-path is to be taken (ISW1=1). Subroutine

PATH2 is called if an sx path is to be taken (ISWl=Z). Subroutines PATHl and PATH2 both call subroutine MODEL which, in turn, calls the specific tire model subroutine to be exercised. A subroutine calling flow chart is shown in Figure IV-1. ci-path I I

.-> .-> dMODEL 1 1 4- 4- NMHS 1 NMHS2 NMHS 3 NhlS Kl NMGDR

1

Figure IV-1. Flow chart for subroutine calling when main program NMDGT1 is used. NMDGTZ. This main program calls all of the tire model subroutines directly. The value of input datum ISWl selects straight-ahead (ISW1=1: a=O) or free-rolling (ISWl=Z: sx=O) operation. As with main program NMDGT1, the swept variable, s or a, is increased according to the initial value, step X interval, and number of steps specified by the input data. Print or plot output is selected by ISW2.

The main programs read the following input data:

ISWl Selects variable, sx or a, to be swept

ISW2 Selects output mode, plot or print

IMODE Tire model calling number I NMDGT1 only NAVE Name of the tire model called (12 char.)J MU0 Static coefficient of friction, uo

AS Speed sensitivity parameter, As

V Traveling velocity hIU X Longitudinal coefficient of sliding friction, v, hIUY Lateral coefficient of sliding friction, p~

GS Longitudinal traction stiffness, CS

Lateral traction stiffness, Ca

Longitudinal carcass stiffness, K,

KY Lateral carcass stiffness, K Y Longitudinal patch point relocation factor,

8, (set=l.)

BY Lateral patch point relocation factor, P Y (set=l.) L Contact patch length, L

FZ Tire load, FZ

SXll Initial value of sx for sx sweep

DSX Step interval in sx sweep

Number of steps, or points, in sx sweep

Initial value of a for a sweep

DALFA Step interval in a sweep bl Number of steps, or points, in a sweep

The following parameters are assigned by a DATA initialization statement in NMDGT1:

ALFl Fixed values of a for which an sx sweep will

be conducted.

Fixed values of sx for which an a sweep will

be conducted.

SUBROUTINE MODEL

When main program NFlDGTl is used, the tire model subroutines are called from subroutine MODEL which employs the following input and output arguments.

Input Arguments (MODEL)

SX longitudinal slip parameter, sx

ALFX slip angle a (degrees)

I MODE calling code number (Table 2) Out~utAr~uments (MODEL)

normalized longitudinal force Fx/FZ

FY normalized lateral force F /FZ Y Xbl Z normalized aligning moment MZ/(FZ*L)

XI A adhesion limit fraction 5,/L

XIS transition limit fraction SS/L

It should be noted that argument XIS is relevant only for the HSRI-NBS-I1 and HSRI-NBS-I11 models as these are the only models which include a transition region between adhesive and sliding contact.

PLOTTING SUBROUTINES

The plotting subroutines NMGR2, NMPL2, NMPL3 are not included in this appendix as they are highly dependent on the particular computing and plotting equipment utilized. -. FORTRAN VA~.~S 15i16i;la IB.JANC/U PACE 1

1 1 f' C~NM~GT1,. . . , . ~~~N.P~QFR!M.~?R.?IGIT~L.TIRC. ?ooE!,s;...... C mmmmrrmm~~~r~mr~~rmmmmmII)IIm~.1~C.IWC,OLI~r)~W~*~~~~~~~~~~~*m**~~*~u C REAL MgOa Ml,JX,MuY ,KXafY IL BIMENSXOM ALF2(5)rSX2(5) COMMON lPR,fRDbfWRaIKEY COMMON A1F1(5),8Xl(SI COMMON sxlir IM~DE,YIA,~~S~OSXI~8~2 COMM~N TSWl. ,SXI,ALF4ItN~~,Jl,J~ ~OMMON XOFG~S?~YORG(~)~~XLE)JC~)IYL~N~S?,XMIN?S"~OXHAX~~I~ + YM~N(S~~YM~X~~I~~X?I~VCS)~N~DIV~~~DSCALX~~~~SC~LY~~~ COVH~N Y(285)rFX(ZBS) ,FY(Z@S)aXMZt2@S1a~A~ECBI COMMON MU06 ASr Va MUX,YUY CQMMPN CS,CAL.FA COMMFN KX,!Y,BXaBY COMMPN L,FZ

COMMON DALFA, f -t (I.? DATA ALFZ/R.a4.a8~al~.alb~/a~~~/8.a~05~~1a~~~a~2/ fPRlS IRbnlS IvlRcb IKFYsb -- - DO I. lslr5 .. ALEI(I)=ALFZ(II 1 SX¶(Tl~SXi?(II XISoP" NMAXo5

I: - - . --.. I...... * .-..-• '*.... .-.. . - - ."..* * C mmm~m~p~~m~~~~~m~m~m~.~wm~~m~~mmmm~wmm~mo~mm-mmm.~~~Omwm~~~~*~*~W C

READ^ IRO,ii@il 1swi a ISN~ r'r t *fie** ISWf DESXGNATES WHICH PATH THE PROGRAM IS TO TAKE ,re.. 6 st**** 1 : ALPH4 PATH C ss***s Z r SX PATH C C ***** YSw2 DCSIGNATES PRINTOUT OR PL~T C rs*ss f o PRINTOUT c ***re 2 r PLQT I: PEAO~IRD, 120~1IM~DE, NAME READ( IRD, l~0QIlMUC),ASrVaHIJX,MUY READ^ IRD. ~~BI~CS,CALFA READfIRD,l~0~)KX~~~,BXaB~ READfIROa I!BB)LIPZ READ( IRDa 100?)8Xl l rDSXIN REAo(rRoarasaiaLciraoALPA,M

C -..."..-r..*.-~-...-....*r-~..--*r*- c m~~mm-m~m~mmm~~mmmmmmmw~mwmmm~~m~~~~m~m~a~mmmmmmm~~~~-~mm-w~~~~ C WRIT F( !~~ajflfl@) ~R~TE(~PR,~~~~~~NAME,MU~~~MUX~~U$,V,AS~CS,CACFA wRITFtIPRa7l~@)NX,UV,BXaRYafZaL CSsCSIFZ CALFAaC~LPA/FZ KX=UX/FZ 143 KYaKVPZ Ifl Nl~l N2rl GO ~h tsa,ha)rrswl C ...... C ~mwmwww~m~mmmmm~~~~w~mwwm~ww~mma~~~mwwwammw~m~~~~ww~mmwmmw~mwmm~ C 5t GO Tn (S~,~ZJ~YSW~ 51 CONTTNIIE WR~TE(!PRIS~~~B) wRlTF(TPR#b@fl@) 5) CONTINUE ALfAIzALFl (N:) ~(~I~SXl! CALL, PATFl- 60 Tn (?1#72)tISw2 72 CONI~NUE IF~ALFAIJ16@, lh0r 15!2! j6fl CALL NHGR2 1SB CALL NHPL2 71 CQNTXNUE Nl?rJ1+1 ?B(N!-MMAX~S~~~kfl# la@ C ...... C wmwm~mmmm~~mmmw~~m~mmw~~wwmww~~mm~~m~mmm~amwam~w~w~~wm~~awm~~~~~ C 6f GO ~h (6(,b21,ISWZ 61 CONTINUE WRX~E(IPR,~O~O~ WRXTt(IPR#bBflF) 65 CONTTHVE %X 113x1 (F2) X(l)rAlPIl CALL, PATH2 GO TO tifllrl~Z!tISw? CONTINUE IF(SXI1130,l~@rilB ~URCALL NMGR2 33fl CALL NuPl2 I@!COYTrNIJE WZ:N%+ 1 KybM3*MPAX)bP#ABr lG0 CALL EY:'? P I", ...... a L ~~~~~~~~~~~~~~~~mmm~mo~mm~mwmwmmwmswqww-qemwmmm-mw~mwmamn~wm~~*~ P FORMAT~?F~;@,ISI llae FORMATtSEBqS) IZfd! FOR~ATtltrbA31 1201 FORMATfZI1) 5PaR FORMATflHlI ~RAR~ORMAT(~~X,'SLIP ANGLE LONG, SLIP ~ORCF.LONG F~RF~-L +A U~~~~~'tll~#~~(~~~~~)~~~X#UH($YI#~~XIIW(FX],!~X#~H~FYIB ~~~X~U~~M~~/~~X~~H~EG~E~~~~!~TH~CRCFNTIQ~~~L8.t7xt8HlVW l.0 ~~x,~~H~~~~,LR-!N!~~x~"I~L-----*~C~~+~=~+~a rrmw-~-rr)* + rmm*wrrrra mawwwm-=mm~/i i) - ". - FORTRAN VB~,13 ¶)i16120 I~WJAN;~~PAOE 3

RLSCI( LENGTH, ~AIN. 9si (Q)BW~Z)* ,$%$9. 1827 (fl071fl61 - - r*COMPfLER -*or* CORE** PHASE USE0 FRFE DECLARATIVFS 08622 14203 EXEClJTABLEs @a335 13530 ASSEMBLY 01585 17928 - - T FORTRAN ~@6,i5 1li39136 !@*JAN;~~PAGE I

i.** LrrK PA~W~OF nrlN LINK NMDGT 8UbROUTINE PATH1 REAL, FIUO, MUX, MllY, KXr KYr L CQHMPN IPR,IRDrlPR,IKEY COMMON ALFj (9) ,Sf1 (51 COMMPN S~~~,~HODF,YIL~YIS~~SX,!S~Z CQVMON 18W1, ,flXrrALFAf,N,Wlr, J1, Jt COMMON XORG-) ,YORC(S) ,YLEN~S~,YL~N~S~,XMIN~S) ,%MA%($), + YMIN[Sl,YMhX(5~ rNXPIV~S1,NYDIVIS!I~CALX(!!I ,$CALY(S) COM~~NXIZBS)rFX(285)rFY(Z@SI,XMZ(2flS) ,NAMEt6) CQMH@N MUQI A$, V, MUX, MUV COMMPN C8,CALFA COMMON KX,KV,BY,flV COMMON LIFZ COMMON. D&PA DO ,?0 T+l#EJ CALL, W~DEL(X~I),ALFA~,FX~I)~FV~I~,XHZ~~],X~A~XTS~IM~DE~' CO.TO (8flr9431rISW2 $R WRITE (~,?BR~)I,ALFAI,x(I~,~x~I~,cY~!),xMX14,XIS 9? YtIti)eX(I~+DSX R~BOFORM~T(I~~SXIF~,~~~QYI~~;~, ~X,?F~S~UI 70 CONTINUE RETUPN PNn

ROUTINES CALLEO: i"0DEL

~~COMPILFRm;-;r C~RC** PHASE ugeo FREE OECLIRATIVES 81255 15618 EXFCUTABLES st183 13602 ASSEMBLY 01297 l82fl8 .+ -. FORTRAN ~0b.13 lli4fllfli 10aJAN-74 PAGE 1

C**** LINK PATH2 OF MAIN LINK NMDGT SUBROUTINE PATHZ REAL, MUQr HI,IX, HUY 0 KXr KY 8 L COHHPN IPRol~Or~~RoIKEY COMMON A~F~(5)08X115) COMM~Nsxii, IMOD~,XIAOXIS,DSX, IS~Z COHMPN ?SVl rSXfrALPAIrNoM,JlrJZ

COMMON XORG~S~OYO~G'~~),XLE~~~S],YL~N~S?IXM!N~S~OXMAX~~~., . +. YM~N[5)~YM~X(5),~%~IVI5I,N~QIVI53~SC~IX~SI,SCALY(5) COMMON X(2091 pSYk2041 ,FY [2B41 ,XMZt2BJ51 pNdMECC1Pi COMMON MUOId~rVeYUX~qUY COMM~NC8 s CALF4 COMH@N KX,UY,BX,RY COMHPN LlFZ CONMbN OALCB 00 1BB, IalrM CALL, M?D~L(S~I~X~I),FX~I~~FY(I),X~~(~I)~X~A~XIS~I~O~E~ 60 to f116,128¶oJSWZ iie w~r~c~~,saaa~~,x~~~,sx~,~x~~~,~~~~~~x~i~,xI~,xrs Bpi?@ FORM~T(I~OSX,F~~~O~~XOF~~~O~X~~FI~~U~ d2fl X(I+l)nX(Xj+DALPA 10P CONTlNUE RETUPN FND

. . ~~COMP~LFRII--~ C~RE@* PHASE FREE DECLARbTTVFS 01255 13610 EXFCLJTABLES all83 13682 ASSEMBLY $1297 l82fl8 -. * FORTRAN VBh, 13 flillrt40 ~BPJAN~?~PAGE I

RL~CK LENGTH !ODE!- jjl~ r sagbu4) * ,Jlt$. 1027 (ff871fl6)

*rtOMPILfR mar;* C~RE** PHASE 1JSt-D fRFE ~ECLARAT~VFSBflBQ2 14063 FXECUtARLEd Wg996 13899 Q13SEYBL.V Brtc3rfS tft4952 w .. - FORTRAN VB~,13 i ii09i02 I BI JAN;?^ PAGE 1

t't C*NM~GT~:,,,..?A~~.P~OGR~M.P~~.O~GIT~L.TYOOECO; ..-.... -. C mm~~m~~ma~momao~~mw~o~~wwma~m~a~~ammm-m~~~~~~-m-mww~-~~~~ew~-~~ C REAL MU04 MUXI MIIY ,KY, KYI L COMM~NIPRI IPD, IWR~IKEY COMM~N A/$! (3) ,$U1(5) COMMON 3%1;, ~~ODC~XXA,XIS,DBX,18~2 CO~M~NISWI. #SX~IALFAI,N,M,J~,J~ COMMON ~ORGJS~~YORO~S~,YLCN~SI,VL~NIS~,XMIN~~I,~MA~~~~,

, +, YHZN(5) aVMbX[!5,, NXQIV(5) a NYDIY(S¶ ,8CALX(91 ,aCAL'f($) CO*M@N X(~@$~,FX(~~~),FY(~O~)IXMZ~~BS~INA~~~Q) COHMPN MUO, AS#VI MUYa MUY COMMPN CBrCALFe COMMPN KX#$YaBX,BY CQMMOFJ L,Pz COMMON OILFA

c . - . ... .-.di...... "..*-. .,.. ..-..-*-.- .*. I-"r-" . -. FORTRAN ~06.13 iiisgr4~ tem~~~-tuPRGE i

QCB43 GO tb ?0b nau4 tar CALL, N~~~~~~~II,AL~AI~~x~II,cY~I~,x~~~I~,~~A,~~~~ BBUS 00 TO 206 Pl0Ub EB~CALL N~H$~~X~I~~ALFAI,~XII~~PV~I~,XMZ(~),X~)~,X~$) @0!7 GO fh 286 @@48 20. CALL N~SKI(X~I~~ALPAI,FX(I~,PY~I)IYMZ(!~IXII~~ a049 SO TO 286 %0$ CALL N~c~R~x~~),ALPA!,Px~I~~?Y~I),xMz(~),xIA~ 809 1 306 CONTJNUE a052 GO TO (O~,~B),TSWZ gej3 00 W~~T~~~,~~~~~I,AL~AI~X~I~,~X(I),~Y~I~,XF~I,XIA,XIS n844 90 X(!+llaXtI)+OSX fl0SS 7fl CONTXNVE,. _ GO TO (71,12)rf8wZ 9057 7i COuT!NU€. a058 ff (1~0~~~1)160rlb0,150 q~!59 jba CALL NMGRZ P0bB 1SP CALL NMPL3 e061 71 CONTINUE a062 GO TO 20Cll0

c . . - . . * . . . .-. r . +.. . r-. . r ...... --7 . *'* C wwmw*m~mw~~~ma1wwm~~I.Im~wmIm~mwwwCL*-.)C~m-~~.I~m~*-C~-~~-~-~~~-~ c a043 00 TO (bit62),~sw2 P064 61 CONTINUE eebs walr~cl~a,jaee) fl0hb WRITE(?PR,bB@B) P861 bj CONTINUE Re68 SXfmBa g0t$9 x(llr~~ri1 a@?@ DO la! IMODE~lrS @071 DO I?@ JsirM ge?z GO TO (~~7,2~8,2~9~~i~,2il1~!MODE @0 3 207 CALL, NMH#~~~XI,X~I~,PX(II,FY(I~,~M~(!),X~A) 9074 GO TO ?12 ~10~s EBB CALL, N~H~~~SXI~X~I~,PY~I~~FY~I~,XM~~I~,X~A,Y~~~ QB?~ ~c TO 212 (a017 $09 CALL, N~H~~~$YI~x~~~~~%(I),PY~~~Ix~~(~~~x~A~xI~~ n07R 60 To 212 flS79 2113 CALL, N~$~~~s~I~x(~~~Fx(I),FY(~)~x~~~!~~K~A~ grad^ co rn 212 PBP l $li CALL N~oER~sYI~x(I),~x~~?,CV~I~,XM~(I),XIAI orewr 312 CQNTJNUE, PgP7 GO TP (I~B,~~R),~$IL RQrtld YCIT~(IPD~SPRB)I,X(I)~$XI~PX~~~~FY~I)~XMX!A,I!$ @sng !?a Y(~~~~SX!%~+~ALFA 6 is9 CONTJYIIE @a87 GO TO ~l!lfrlAZ),TSw2 @$08 bi COPTINUE. age9 - JF(IMODE~~)~~B,IU~,~~~ flflO@ I4@ CALL NMGR2 BIB91 t3fl CALL NMPLS 41092 la? CONTfNUE BIP193 ZB0@ CAlL EXIT C - ". 11 h19i~2 IB~JAN;~~PAGE 3

. " - . r . .-.. . r...... r. ...r. . . ..* . ..- . . . . 1: m~m~m~mmm~omm-m~m~v~m-m~mmm~mum~~~mw-~mmm~m~o-mm~~vam~em~~e~~mo C ieag FORMAT~~F~;~,11) li00 ~ORMAT(5~8a3) lZ0g PORMAT(ltrbA3) 1201 PORMAT(ZX1) 5@0fl FORMAT!lHl) 600e PORHAl(leX,'SLIP_ANCLE LONG, SLIP FORCEmLONC F~RCE~L + # ~O~E~T'/)~X,~H(ALP~A~~~BX~UH(SX),~~XOYH~?X)~~~X~~H(~Y)~ +! I~~~H~M~)/~~XI~~DEO~~C$~~!!~TH~I:RC~~N~I@X~~Ll, r /XtOUIf!OIj LB +bXf1gHle?0.LB*!N!16XL'tm~~~*,?-?~ *m*-wm*c** *mr-wwl~mmr , + *wmmr-~mwmaj amapmq--*mf/* *)- , 8RBB FORMAT(IIO~X.T~~ZI10x0 ~6; 31 fxn~~9.5~4j . 7R8R FORMAT($X~(~~08: ,~4~2~ OX. c~~~s~,f4ri!B4~,*~~~@@,~~,2##, + 5x0!V *'OPU~~~UXO'ASr*BF5a3//B + SXc!CS ~*,F4,~,4X0CCALP~*t,f4.11) ?(AR FORMAT~JX,'K% U'~FO.Z,UX, 'KY a*, F4,2,4X, + 'BX ,P~oPS~~~~XO'BYar,FSa3/f, + SXI'FZ ~*oF~m2r~X,'Loc0FSe3//) c ..--"..-*.-*..,...-. - ..-.-.-..-... * C ~mmmmmmm~~mmmwmmmm~ma~~-mv~m~~m~~rmrcm~~~~~~~~m~mmm~~~mmo~~~m~~ C END FORTRAN VBh, i3

t r

i ...... +. . ... g . --.. - . . . . . - . - ...... - . - . C m~~~mm~m~m~~~m~wam~.~mm~mm~-mmw~w-w~-m~~~m~~-~mwwm-~~~~a-*mm~-*~ C ~2~0: AI.F~ALFA*.~~~~~S~ SY~SIN(ALP)/COSIACP~ !F(SN)zl#23,21 23 1PISr)?1,2?n?1 21 FXaca, FYtBb XIAr,l. GO TQ 30 2i CouTTNyE - rrtspc.)rr#le.s~ 81" SXg1. 2fl VSEV~C~S~A~F)*SORT ~ARS~SX)**~.~AOS~SYI**?. 1 MU=MUO*(~,WA~~VB) TEMP~sQRVEI~~($XICA)~.+A~S~~~*~ALFA~**~,1

C.."", ' OETERM~NEADHES~~N RANGE; m ROUT~N~SCALLED~ SIN a COS , SQR? r A89

*~~OHPILERIR-~;W C~RE*~ PHASE Usha FREE DECLARITXVES 80622 14243 EXECUTABLES Elf967 13898 AS8EMBLY BtlR5 18320 t'f 1 te~~asi.,. ,. ,nv?i 2.YB~. TJ~c~~~o!L.~.~~:c~. PC6, .RCF~ ...... c ~~~~*~~~*~~mmm~am~mmmmmmmmmm.)m~u.)(~~m~*.)~~~mm~mmmmm~m~~mme~m~~wma c SURR~UTINE N~WS~~SX,ALFA,FX~PY,M~,XIA~XI~~ C ...... C *~Pmmbm-mmmmm~mmm~C~mm~~~amC~~~(~.)mm~~mm(I)mm~~-~mm~~qmmmmmmm~~-ma

C, ,,- c.. .. .co~~ici~-SLI~IBG PQS~IBLE ONLY, AT WHLE~LOCK: C WHEEL LOFK FORCES ARC COMPUteD, c TRAN~ITION FROM ADHESI~N TO SL~OING. C UNIFORM VERTICAL PRLSSUR6! bI9TRIRUTfON C ...... -.., ...... -..... t WmmO~~~~~~@*~~Ob~~~~~'ILC.)U~m.)CI.)~W(.I~1I.~-W~OV~~~~~~~~~W(.W~Wmm.)~ C REAL, MU,MU~,?Z~M~A,MZT#M~S,MZP,K~,UX~L,MUX~MUY COHMPN IBUFF(1799) COWM?N HUOI AS, Ve MUX, MUY COMMON C8,CALCA COMMON KY, !Y n0XtBY COWHON L,FZ C ...... ~...... C mmmmmrr~~~~rmamrmrm~mmmmmm~m~~wWm~m-.)~I).I~m~~(Immm~~mm-~~~~W~~~~~ c ALFI?LFI~.~I~u~~~~ 8Y~SINlALPl/COS(ALCI IfSSK)t1,29,Ll 23 XPl3~)2lr22~21 22 PXbBr FY@0, MZg0, XIAoa,. xxaq .- go rc us ri COWTINUE rrtsymi.,ii,ie,zh 2@ SXp1. lfl $P~SQRT(~A~S~SX)**~.)tt~~b18vl*~?.?) V88V*cO3iAbf *8P MUpHUOt ( 1 .mAB,V81 I$ISX~ln)3An15r2E

C*, t c... ..COMPLETE S~IOING(WHEEL LOCK?. C IS YXAaq, XISsQ., X & AP=Bt XISP@bF1. $XPs@, sYP0p.- GO ra lei ", , C.. ...DETERMINE ADYESI~~NAND TRAN~ITXOY ~IMIIS: I x L>U * inx 8 0 -a- I > Q)(* * 8 V) ask- 0 C .xi- 18 n ma- n tech Q 9 a r -+urn g) *I wi *.a .M b E f bL-a W I m >NU3 r I a 4 rn >.r ? . rn k U.fW 14 8 x \-a Y r C --a- * * I m rr 8 - .;t - c.+ n a W u a*& V) I 6-- e * YEOU *cr I 4 tU n 4 n I a * a IL -(\X .* + I * 6 A n I h h .+I 4 Qo'Lr an * 8 4 0 X O (em U I .a h u %a e -%- \ I P- A w a -m XQ,* .r .I 8-0 x m3 9 **a c * a ZUOJ a w 9 a-cn r I -a\ b x o ,<--\ u B 3)- - U1. Y 4 wb~) IL 8 98 rr: u f I C * . %.A43 2 * I 19 - h. u x h • a<* a a I+ m 2 C- . U a n CL.U3 :U * I m ( a * QD 4 x*x \ C 'u n e. \ k wan* ,r • \ P > X *Urn 4 I - • .W '8 +- - r e 0) ~3 +I n.~, Cc-4 U \ a - >\+ * I W .-.+ 4 X 3 4 43.r- 3 * B --mm #- V) s ie urn- IT* I i a a+u z a c A SC~*k a I - UX\ 0 3- -yI- 4 -U8 -1 1 -a -he , v x m 'RL *a U a Q)X - 0 I " -*-' * u3 4.b s LX(R \LA J * Ic U \.u 6 ,6 Z , *tCCk *a.. w UJ JWlk X 4t\ @ a-ra o d - (U ex a4x o UUIX tnna Q I * w w -0 - i.r *-+.I 4.- I .u UrCCI* .-WN Z I m C5 a-x I B V) *a - ux a e.- CXI u B NN .-me36 o rC 6 w e.41- X *I+ a Q). +.N h \. +. 18 1- 6 Y) mmyl .. m u uu-w *QUB x OR+ c.ts>a N @ 6: - - us - a kx.I x Q a~ .--a .\(LI.DU lk I QUd5 fi a o X~QL>UJCLL * -4-4 ~DI rrl XCQB .u *.w&n CI .o. &L 9 OW.+ B) 9 an.+ .m * w.- m%++ i> s - t &L5: -omn n OX\+ c-\+ 9 ~CX=YB- m J a Q Ow- e33- 19cr- VWJ s lu xmxx -DL.=> .Q a= 3.x.w a +a -C z QSXU BX4UQwe ma433 Z m*c*,t LLJ-RL O EKE ). NNN a \W O % s i- 8 wtcd-X.h &.c*e-+H .b- *-.+ 2- *-+ -4 4 \13 Ift+ 2 LIIII - ~)rnme~desxx 8 x x COU~U 4~3e- 9x--anu- n arm a z 2 V, a,4.~aan~~~nu.c~,-BIa.c,oo u rr u-rx uux, -,-.cnra--~~~'U XPW +I Q - G )4tu nmrn~nn+ac~~t-~~n+~~w unmk nna~ smrro-xnnz + hi~r r 3 \ &aD 14awam . .-am -Q) R- *+mm ~C-I)U ao-b-re~am A mar 91 +C I1 I CC. 4 WUwOUUO~UHOk~+?O+Q~W XXXX )t*) NU'NtUX'NWN 3 XU 8 WZ ~-x~~x~cs~~x~3cx~0xxo IL~L~LLL~~L ~~CLXB)XLEII I .a ah (0 wl C( -.rrun 2 r - 6. Ct6 U 6 G . - 6, . 6 .c YlnJcR - &n 9- UJCP d - Q r =r Cl(nYI 13 :d • C- .OXYz 4 - -. 6% . O JIM > .UUU U U UUU .UU U -C m 2- -

-OD Q-Q zaw 6 - " lii13113 ~BOJAN~~UPAGE 1

L SURR~UTINE NMH~~~SX,ALFP,FX,FY~M~,XI~,XIS)

F . - ....- ..."..* *.- . - ..-... . . - I-. r.. - . - .-.. - c c~mmc~~~mw~~-mm*m~~.~nmmro--m-mm~~)mw~)~)--mmom--m-~~-~mmmmmmwr~mm~a C b., ,.* c.. .. .COMPLETE SLIP IN^ POSSIRLE ~NLY,AT WHEEL COCK: C WHEEL LOFK FORCE8 ARF CONPUTEO. I: TSAH$ITIQN FROM ADHESION TO SLIDING, c PARABOLIC VERTICAL PRESSURE DISTRIRUTI~N: i * . . - - ..* --.r.. - . . . .-. . . . -... . r r - . - . .-. t r-rmrmm~~~r~mrm+rrmwmm~.I,-~~~~CCm~mwcw.)m(Im~~-m~m~-m~-~am~-a~~~-m C L REAL MU,WUQ,MZ~M~A~M~~,MZS~MZ?~K~#UX,L~MUX,MUY COMM~NIBUFF( 17991 CO~M~NMUO~ A?, v, ~uu,~uv COMMON CSr&ALFA COMMPN HXI~YIBX~BY cowahi I,FZ c ...... -..*.. r r . . r.. r r t.. .'. . r r...... C ALF~~L~A*.~174533 SYmS!NfALP)/C83(ALC) IftSX)~l023~21 28 TF(S/)21.22rZl 22 FXeld, PYe@, HZ010, XIArI, XISrl" 60 70 999 zi CONY INUC IF(SX.I.) IR,IB.IB 2fl SX81. la SPwSQRT($X*$Y+9Y*SY) VSEV*COS$~CF)*8P MUeHUQt ( 1. IA~~*V$Z ~FISXWI,)3a, 1~~22

Ct I Fm.,..COMPLETE SLIDING (wHFE1 LOCK), e 15 XIAofl, XfSaP,, Xf hia3gjp XT$;Pa@, $X"%P, ~Y~PP,, GO to 1Zfl c, t C.. .nETERMlNt ADHESION AND TRANSTTIO* LIMITS: * .. -. 7ORTRAN V06.13 ililfil3 lea JAN.74 PAGE 2

TEMPrpQRT t iAg$j$~*~8)*~~;)~(ABSCSY*CALFA~**~; 11 XIA~~,~TEM~/(S,*~UO*fl,~) XIS~I..CS*CALFA/ ~CI+CALFA)*SP/~S~*HU*(I*;$XI ) c rrtxZs)s~,3s,~e 35 XIIPlflr XISPrR* GO Th 128 c 4a ~rixi~)ts,~s,ss 45 XIAPtg. XIASP, 60 TO 9Fd c SA IF~~~~~IA)~B~~R~?~ 6fl XIAP81r xrtwpi, GO TO 1Pfl c 7A ~F~xIS~XI~)~~,~B,~R 8fl XIIPrXIA XISP?XXAP GO TP 128 , . - 98 IF~~~~XXS)~B~~lantiim 10P XIAPaXJA XISPatL GO ~b 128 1lR XIAP8XfA XISPIXJS a 'Cm.... ' COHPUTAIIONOF IRA~T~ONFORCE* c 12~FXI~CS~$XP*XIAP**Z~ PXT.( 1a~~.?~$*~~~*~3~~~,*~~~~m~~~~1~~~~~~(~.~~l~~)t t~U*9X/8P*(~,-2,~U!~C~XIAPl~X~S~)*tX13P~XIAPl PXS~MU*$X/SP*(!a*3a*YISP**ta+Za*XISPfi*IaI PXn PXA+FXT+FXS

'Caasaa ' con~urrrron b~ E~RNERING F~RCE: C FY~~cA~$~*sYP*xIAP~*~. FYI.( I./J.~~!L~A~SYP~(~,~~~IxIAP~x!~P)?xI~P/~~~~xIAP~+ +~U*SV/SP*($,~2L*~I$P~XIAP~~XJ8f)*(X13P*XIA~) FYSSMU*$Y/$P*(~~~S,*XI~P**Z~+~~*XISP**~~) FYI FYA+FYI+FYS c,, c.... .COMPUTATIONh~ ALIGNING MOMENT'. c HZAS~./~:*$XP*~Y~*~CS.CILFA~~XIAP**~;-T~/~~#$YP~~CA~F~ + *(u,rXfAP**S,r$,*XlAp*?2a 1 ~ZJ=~Y~(~S~CALFAI*~S~/~(I,=SX~~*~~I*XI~P~*~,~~~~~-YI~P~**~~~ +*~~/~S~*(~~*~~~P**~~+~~*XIAP*X!SP+XS~P**~~~~~~*X~AP~~~*X!SP+~~~) +*(XI8P~XIAPl. . ~zTB~z?+sY*~c$~c~LFA)*~~xP*Hu/$P~[~a/~~+~.;~~~~~)*~~~~*#~~@/~ 1;~ +XIPPJ*, l*(f~*X!8P**2~+3m*XIAP**Za+4~*XIAP*XISF~10a*(XIAP+XTSP~+ +lB,))*tXT8P.XIAP~ .- "...I !1;13;13 10mJAN*70 PACE t

- C 099 RETURN EN0

ROUTINES CALLEO; SIN ,CO$ r8QRT #A88

RL~CK - LENGTH- - tNMHS'S 8 140 (BB4358)fi ,$s$$, 1825 (afl71R2)

+*COMPILER mi-;r cb~~r* PHASE [JSlED FRtE bECLdRAT!VLS 8e6G2 14063 €Xt!CUTABl.ES tIj.387 13418 bS9EMBt.Y 01393 18112 "t r c.. ..COMPL~T~ ~LIDYNG POSSIBLE WITHOUT WYECL LOCK. C WHEEL LOQK-(JXS~~ICAN 0E 8PECIFJE0, , c NO TRAN~~TTONFROM ADHFSTON t0 SLI~INC, c ...... C ~ow---r~maw~-~a~-mmmmmm-~~~~*wm~rlim~r-m*~m-m~wm-~~~w~m~~~~m~~~~~ C REAL, YUO, MUX,HVY, ~i,KYPL, KX COMMPM IBUFF(17991 COWM?N nUOIAQsV,MUX~MUY COMMON CSetALFA COMMPN KX,!YIBX,RY COMMON LeF2 e ...... ,...... I...... C r~~~oo~m~~mm~rmrrrrmm~mmmm~pm.~~mmmw-m~.~-~m~~~mm~~m~~mmm~wm~mm~~ c ALFmALFA * 3: l~lb/i0@. SY~$1N~ILF)/~QS(CLFl !F(SXm! la, 17,1? 17 Y1A.P. JXst* SPESQRTti~isisx)*~i,~+i~~sis~~~~Z.~) GO, TO g0 _ _ 1F fPfSXll6,llrbb 11 ~F(8~)Ibrl~,lb 15 FXxB, fYm0, MLIBI XIAa1.- GO TO 20 I6 CONTIINLIE* 3XPs3X/(~,~Sxl SYPaSY/(1,-SUI SP@SQRT( (ARS(SX~**~.~+(ABS~$V)C*~.)) c,, C,.,..DETERMIWF ADHESION LIMIT: ...... FORTRAN ~06.~3 iliiir~~ ~B-JAN;?~ PAGE Z

I* 7t4 CXPCS~SXP*~IA**Z~+~UX*~B~~~P~~~~~~XIA)**~.~~jei~,*~I~l ~Y~S~~LFA+CS*SX)*~YP*XJI~**~~+HVY$(~YISP)~(1 e?XIA)fi*Z.*t I;+~.*xTA' , MZm,)b66*8VP? 13e*CS*SX+C~L~A*(3et4e~~fAl1 *XIA**Zfi + +~S*(?Y!S~)*(~UX*SX*(I.+S~RX~A)~J~*MU~*Y~A)*(~,~X~A~*~~~~%~~ + +rX?FV/(KV*L) GO TO 20 c,, .. .COHP~ETL SLIDING c uo ~X~NUX*SX/SP FY~MUY~IY/QP, HtgFY*FY/(YY*L) C r ,. c... . . HUCT IPLY BV FZ AND L'. c 2~ FXPFX*~? FY aFY*PZ MZIMZ~PZ~L

C . . I r...... +. r r .. .., . r-r . r . +., - + ... + . . t r-r-rrrr-rmrrmm~m~~~m-m~~m-mmpmpa~~~~.il.~mmmmm~~~-m--~~.mmm=~~mm-- C RETURN FND

. *rCOMPIC€R r-a-a CORFII PHASE USFD FREE DECLARATIVF3 8e8F2 14043 FxEcurreies ~1~8713638 AS3EMBLY el217 1~268 FORTRAN ~nb,i J

b,, t.. ..C~YPLET€ SLTDING rOSSIBLE W1THOUT WHEEL LOC~. C WHFEL LOCK (9Xglcl SHOULD NOT BE $PECIFIEDn C NO TRANSJTION PROM ADHESION TO 8LIDIN6, C . " - . . . . " . - . - - .,-. - . .-*-- *.- . - . . .-.- - - C mcmmm=mewwm*ammmo=a-mm---mmwmmao-m~mc-mbemm~mmqmowm~a~eo~~m~m-m c REAL,MUO~ nljr, MI!Y,M~,HY. L, KX COMMPN IBUFPilP891 COMMON HUOIA9,vr~UX,~U'f COMMON CSr CALPA COMMPN KX#(YBBX,RY COMMON LBFZ

e - . . . . . - - . *.- . . " . .-.. *.. .a. . - . . . -... C mmo~m-mmm~~~-mm~mw~m-mmoa~mm.~mmmmmmmam~am~~mmmmmawm~~m~~-mw~~mm C ALPSAL~A*.~~~~~SS $Y?SIN~ALF)/gOSt4L*l - ~P(8~nf#)lfl~~i?#15 15 FXn0, FYo0, MtoB,, XIAq,- GO fn ze ii sxt.9~- - h. 1g IFtSw)l6~11~~6 11 !F(8Y)fbr1~rIb 16 CONTIN!JE_ , SXP~SX/~~,?SX~ SYP~SY/(l.rSX) TE~P~SQRT(A~~(SX*CS)**~~+ARS~S?*CALPAI**~~1 c ,., 6,. .. ,OETERHTNE ADHESION LIMIT", \- .". FORTRAN VB~,i3 1iiiiid9 f @rJAN~?U PA@E 2

C , ,., C,,...COMPLCTE BLIOING c PA FX~CI*MU~*SX>TFMP ~YEC~LPA*MVO?QY/TEHP MZ8 .~~~~~~*~C~~CALFA)*SYP*S~P C,, c.. ,..MULT~PLY BY kz AND L',

e RETURN END

-. *~COMPIL~R*-t=- C~RG*~ PHASE USED FREE DECLARAT!VF~ Be688 14843 FXFCUTABLES Biz27 13638 ASSEMBLY BiZGJ 183(118