SASO ISO 80000-11:2020 ISO 80000-11:2019

Quantities and units - Part 11: Characteristic numbers

ICS 01.060

Saudi Standards, Metrology and Quality Org (SASO)

------this document is a draft saudi standard circulated for comment. it is, therefore subject to change and may not be referred to as a saudi standard until approved by the boardDRAFT of directors.

Foreword

The Saudi Standards ,Metrology and Quality Organization (SASO)has adopted the International standard No. ISO 80000-11:2019 “Quantities and units — Part 11: Characteristic numbers” issued by (ISO). The text of this international standard has been translated into Arabic so as to be approved as a Saudi standard.

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Introduction

Characteristic numbers are physical quantities of unit one, although commonly and erroneously called “dimensionless” quantities. They are used in the studies of natural and technical processes, and (can) present information about the behaviour of the process, or reveal similarities between different processes. Characteristic numbers often are described as ratios of forces in equilibrium; in some cases, however, they are ratios of energy or work, although noted as forces in the literature; sometimes they are the ratio of characteristic times. Characteristic numbers can be defined by the same equation but carry different names if they are concerned with different kinds of processes. Characteristic numbers can be expressed as products or fractions of other characteristic numbers if these are valid for the same kind of process. So, the clauses in this document are arranged according to some groups of processes. As the amount of characteristic numbers is tremendous, and their use in technology and science is not uniform, only a small amount of them is given in this document, where their inclusion depends on their common use. Besides, a restriction is made on the kind of processes, which are given by the Clause headings. Nevertheless, several characteristic numbers are found in different representations of the same physical information, e.g. multiplied by a numerical factor, as the square, the square root, or the inverse of another representation. Only one of these have been included, the other ones are declared as deprecated or are mentioned in the remarks column.

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SAUDI STANDADR SASO ISO 80000-11: 2020

Quantities and units — Part 11: Characteristic numbers

1 Scope

This document gives names, symbols and definitions for characteristic numbers used in the description of transport and transfer phenomena.

2 Normative references

There are no normative references in this document.

3 Terms and definitions

Names, symbols and definitions for characteristic numbers are given in Clauses 4 to 9. ISO and IEC maintain terminological databases for use in standardization at the following addresses: — ISO Online browsing platform: available at https://www.iso.org/obp

— IEC Electropedia: available at http://www.electropedia.org/

4 Momentum transfer

Table 1 gives the names, symbols and definitions of characteristic numbers used to characterize processes in which momentum transfer plays a predominant role. The transfer of momentum (ISO 80000-4) basically occurs during a collision of 2 bodies, and is governed by the law of momentum conservation. Energy dissipation can occur. In a more generalized meaning momentum transfer occurs during the interaction of 2 subsystems moving with velocity v relative to each other. Typically, one of the subsystems is solid and possibly rigid, with a characteristic length, which can be a length, width, radius, etc. of a solid object, often the effective length is given by the ratio of a body’s volume to the area of its surface. The other subsystem is a fluid, in general or gaseous, with the following properties amongst others: — mass density  (ISO 80000-4);

— dynamic  (ISO 80000-4);

— kinematic viscosity  /  (ISO 80000-4), or

— pressure drop p (ISO 80000-4).

The field of science is mainly (mechanics). Characteristic numbers of this kind allow the comparison of objects of different sizes. They also can give some estimation about the change of laminar flow to turbulent flow. DRAFT

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Table 1 — Characteristic numbers for momentum transfer

No. Name Symbol Definition Remarks

11-4.1 Re quotient of inertial forces and viscous forces in a fluid flow, expressed by The value of the Reynolds number gives an estimate on the vvll flow state: laminar flow or turbulent flow. Re; where  In rotating movement, the speed = ωl, where l is the distance from the rotation axis and ω is the angular ρ is mass density (ISO 80000-4), velocity. v is speed (ISO 80000-3), l is characteristic length (ISO 80000-3), η is dynamic viscosity (ISO 80000-4), and  is kinematic viscosity (ISO 80000-4)

11-4.2 Eu relationship between pressure drop in a flow and the kinetic energy per The Euler number is used to characterize losses in the flow. volume for flow of fluids in a pipe, expressed by A modification of the Euler number is considering the p dimensions of the containment (pipe): Eu ; where v2 d EuEu ; where p is drop of pressure (ISO 80000-4), l d is inner diameter (ISO 80000-3) of the pipe, and ρ is mass density (ISO 80000-4), and l is length (ISO 80000-3). is speed (ISO 80000-3)

11-4.3 Fr quotient of a body’s inertial forces and its gravitational forces for flow of The Froude number can be modified by buoyancy. fluids, expressed by Sometimes the square and sometimes the inverse of the v Froude number as defined here is wrongly used. Fr  ; where lg is speed (ISO 80000-3) of flow, l is characteristic length (ISO 80000-3), and g is acceleration of free fall (ISO 80000-3)

11-4.4 Gr quotient of buoyancy forces due to thermal expansion which results in a Heating can occur near hot vertical walls, in pipes, or by a change of mass density and viscous forces for free due to bluff body. temperature differences, expressed by

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No. Name Symbol Definition Remarks

GrlgT32/ ; where The characteristic length can be the vertical height of a hot V plate, the diameter of a pipe, or the effective length of a l is characteristic length (ISO 80000-3), body. g is acceleration of free fall (ISO 80000-3), See also (item 11-5.3). αV is thermal cubic expansion coefficient (ISO 80000-5), T is difference of thermodynamic temperature T (ISO 80000-5) between surface of the body and the fluid far away from the body, and  is kinematic viscosity (ISO 80000-4)

11-4.5 We relation between inertial forces and capillary forces due to The fluids can be or . at the interface between two different fluids, expressed by The different fluids often are drops moving in a or Welv2 / ; where bubbles in a liquid. ρ is mass density (ISO 80000-4), The characteristic length is commonly the diameter of bubbles or drops. v is speed (ISO 80000-3), The square root of the Weber number is called Rayleigh l is characteristic length (ISO 80000-3), and number. γ is surface tension (ISO 80000-4) Sometimes the square root of the Weber number as defined here is called the Weber number. That definition is deprecated. Interfaces only exist between two fluids which are not miscible.

11-4.6 Ma quotient of the speed of flow and the speed of sound, expressed by The Mach number represents the relationship of inertial Macv/ ; where forces compared to compression forces. For an is speed (ISO 80000-3) of the body, and p RTkT c is speed of sound (ISO 80000-8) in the fluid c ; where γ is ratio of the specific  Mm heat capacity (ISO 80000-5).

11-4.7 Kn quotient of free path length of a particle and a characteristic length, The Knudsen number is a measure to estimate whether the expressed by gas in flow behaves like a continuum. Kn/ l ; where

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No. Name Symbol Definition Remarks λ is mean free path (ISO 80000-9), and The characteristic length, l, can be a characteristic size of l is characteristic length (ISO 80000-3) the gas flow region like a pipe diameter.

11-4.8 ; Sr, relation between a characteristic frequency and a characteristic speed for The characteristic length, l, can be the diameter of an Thomson number Sh unsteady flow with periodic behaviour, expressed by obstacle in the flow which can cause vortex shedding, or the Srfl /v ; where length of it. f is frequency (ISO 80000-3) of vortex shedding, l is characteristic length (ISO 80000-3), and v is speed (ISO 80000-3) of flow

11-4.9 coefficient cD relation between the effective drag force and inertial forces for a body The is strongly dependant on the shape of moving in a fluid, expressed by the body. 2F c  D ; where D v2A

FD is drag force (ISO 80000-4) on the body, ρ is mass density (ISO 80000-4) of the fluid, is speed (ISO 80000-3) of the body, and A is cross-sectional area (ISO 80000-3)

11-4.10 Bg quotient of drag force and gravitational force for a body moving in a fluid, The characteristic length, l, is the body’s volume divided by expressed by its cross-sectional area. c v2 Bg D ; where lgb

cD is drag coefficient (item 11-4.9) of the body, ρ is mass density (ISO 80000-4) of the fluid, is speed (ISO 80000-3) of the body, l is characteristic length (ISO 80000-3), g is acceleration of free fall (ISO 80000-3), and

ρb is mass density (ISO 80000-4) of the body

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No. Name Symbol Definition Remarks

11-4.11 Bagnold number Ba2 quotient of drag force and viscous force in a fluid transferring solid particles, expressed by d2 Ba s 1/1f 1/2 ; where 2s 

ρs is mass density (ISO 80000-4) of particles, d is diameter (ISO 80000-3) of particles,  v/d is shear rate time-derivative of shear strain (ISO 80000-4), η is dynamic viscosity (ISO 80000-4) of fluid, and

fs is volumic fraction of solid particles

11-4.12 lift coefficient cl, quotient of the lift force available from a wing at a given angle and the The lift coefficient is dependant on the shape of the wing.

cA inertial force for a wing shaped body moving in a fluid, expressed by 2FF c ll; where l v2S qS

Fl is lift force (ISO 80000-4) on the wing, ρ is mass density (ISO 80000-4) of the fluid, v is speed (ISO 80000-3) of the body, S = A cos α is effective area (ISO 80000-3) when α is the angle of attack and A is area of the wing, and qv2 /2 is dynamic pressure.

11-4.13 thrust coefficient ct quotient of the effective thrust force available from a propeller and the The thrust coefficient is dependant on the shape of the inertial force in a fluid, expressed by propeller. 24 ctT F/ n d  ; where

FT is thrust force (ISO 80000-4) of the propeller, ρ is mass density (ISO 80000-4) of the fluid, n is rotational frequency (ISO 80000-3), and d is tip diameter (ISO 80000-3) of the propeller

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No. Name Symbol Definition Remarks

11-4.14 Dn relation between centrifugal force and inertial force, for flows of fluids in curved pipes, expressed by 2vrr Dn ; where  R v is (axial) speed (ISO 80000-3), r is radius (ISO 80000-3) of the pipe,  is kinematic viscosity (ISO 80000-4) of the fluid, and R is radius of curvature (ISO 80000-3) of the path of the pipe

11-4.15 Be quotient of mechanical work and frictional energy loss in fluid dynamics in A similar number exists for (item 11-5.9). a pipe, expressed by The kinematic viscosity is also called momentum plp22 l  diffusivity. Be ; where   2 p is drop of pressure (ISO 80000-4) along the pipe, l is characteristic length (ISO 80000-3), η is dynamic viscosity (ISO 80000-4),  is kinematic viscosity (ISO 80000-4), and ρ is mass density (ISO 80000-4).

11-4.16 Lagrange number Lg quotient of mechanical work and frictional energy loss in fluid dynamics in The Lagrange number is also given by a pipe, expressed by La Re Eu ; where lp Lg ; where Re is the Reynolds number (item 11-4.1), and v Eu is the Euler number (item 11-4.2). l is length (ISO 80000-3) of the pipe, p is drop of pressure (ISO 80000-4) along the pipe, η is dynamic viscosity (ISO 80000-4), and is speed (ISO 80000-3)

11-4.17 Bingham Bm, quotient of yield stress and viscous stress in a viscous material for flow of number; Bn viscoplastic material in channels, expressed by

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No. Name Symbol Definition Remarks

plasticity number d Bm ; where v τ is shear stress (ISO 80000-4), d is characteristic diameter (ISO 80000-3), e.g. effective channel width, η is dynamic viscosity (ISO 80000-4), and v is speed (ISO 80000-3)

11-4.18 Hedström He, quotient of yield stress and viscous stress of a viscous material at flow number Hd limit for visco-plastic material in a channel, expressed by d2 He 0 ; where 2

τ0 is shear stress (ISO 80000-4) at flow limit, d is characteristic diameter (ISO 80000-3), e.g. effective channel width, ρ is mass density (ISO 80000-4), and η is dynamic viscosity (ISO 80000-4)

11-4.19 Bodenstein Bd mathematical expression of the transfer of matter by convection in The Bodenstein number is also given by number reactors with respect to diffusion, BdPeRe * Sc ; where Bdv l/ D ; where Pe* is the Péclet number for (item is speed (ISO 80000-3), 11-6.2), l is length (ISO 80000-3) of the reactor, and Re is the Reynolds number (item 11-4.1), and D is diffusion coefficient (ISO 80000-9) ScDD// is (item 11-7.2).

11-4.20 ; Ro quotient of inertial forces and Coriolis forces in the context of transfer of The Rossby number represents the effect of Earth's Kiebel number matter in geophysics, expressed by rotation on flow in pipes, rivers, currents, tornadoes, etc. Rov/ 2 lE sin  ; where The quantity sin is called Coriolis frequency. is speed (ISO 80000-3) of motion, E

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No. Name Symbol Definition Remarks l is characteristic length (ISO 80000-3), the scale of the phenomenon,

ωE is angular velocity (ISO 80000-3) of the Earth's rotation, and φ is angle (ISO 80000-3) of latitude

11-4.21 Ek quotient of viscous forces and Coriolis forces in the context of transfer of In plasma physics, the square root of this number is used. matter for the flow of a rotating fluid, expressed by The Ekman number is also given by 2 Ekl/2sin E ; where EkRoRe / ; where  is kinematic viscosity (ISO 80000-4), Ro is the Rossby number (item 11-4.20), and l is characteristic length (ISO 80000-3), the scale of the Re is the Reynolds number (item 11-4.1). phenomenon,

ωE is angular frequency (ISO 80000-3) of the Earth’s rotation, and φ is angle of latitude

11-4.22 elasticity number El relation between relaxation time and diffusion time in viscoelastic flows, See also (item 11-7.8). expressed by 2 Eltr r / ; where

tr is relaxation time (ISO 80000-12),  is kinematic viscosity (ISO 80000-4), and r is radius (ISO 80000-3) of pipe

11-4.23 Darcy friction fD representation of pressure loss in a pipe due to friction within a laminar or factor; turbulent flow of a fluid in a pipe, expressed by Moody friction 2pd f  ; where factor D v2 l p is drop of pressure (ISO 80000-4) due to friction, ρ is mass density (ISO 80000-4) of the fluid, v is (average) speed (ISO 80000-3) of the fluid in the pipe, d is diameter (ISO 80000-3) of the pipe, and l is length (ISO 80000-3) of the pipe

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No. Name Symbol Definition Remarks

11-4.24 Fanning number fn, relation between shear stress and dynamic pressure in the flow of a fluid The Fanning number describes the flow of fluids in a pipe f in a containment, expressed by with friction at the walls represented by its shear stress. 2 Symbol f may be used where no conflicts are possible. f  ; where n v2  is shear stress (ISO 80000-4) at the wall, ρ is mass density (ISO 80000-4) of the fluid, and v is speed (ISO 80000-3) of the fluid in the pipe

11-4.25 Goertler number; Go characterization of the stability of laminar boundary layer flows in transfer The Goertler number represents the ratio of centrifugal Goertler of matter in a boundary layer on curved surfaces, expressed by effects to viscous effects. parameter v llbb Go ; where  rc is speed (ISO 80000-3),

lb is boundary layer thickness (ISO 80000-3),  is kinematic viscosity (ISO 80000-4), and

rc is radius of curvature (ISO 80000-3)

11-4.26 Hg, generalization of the Grashof number for forced or free convection in dp For free thermal convection with gT , the Hagen Ha laminar flow, expressed by dx V 1 dp l3 number then coincides with the Grashof number (item 11- Hg ; where  dx  2 4.4). See also the Poiseuille number (item 11-4.28). ρ is mass density (ISO 80000-4) of fluid, dp is gradient of pressure (ISO 80000-4), dx l is characteristic length (ISO 80000-3), and is kinematic viscosity (ISO 80000-4)

11-4.27 Laval number La quotient of speed and the (critical) sound speed at the throat of a nozzle, The Laval number is a specific kind of Mach number (item expressed by 11-4.6).

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No. Name Symbol Definition Remarks

LaRv T/2/1 s  ; where v is speed (ISO 80000-3), R R  is specific , where s M R is molar gas constant (ISO 80000-9), and M is molar mass (ISO 80000-9), T is thermodynamic temperature (ISO 80000-5), and γ is ratio of the specific heat capacities (ISO 80000-5)

11-4.28 Poiseuille Poi quotient of propulsive force by pressure and viscous force for a flow of The Poiseuille number is Poi 32 for laminar flow in a number fluids in a pipe, expressed by round pipe. pd2 See also the Hagen number (item 11-4.26). Poi ; where l v p is drop of pressure (ISO 80000-4) along the pipe, l is length (ISO 80000-3) of the pipe, d is diameter (ISO 80000-3) of the pipe, η is dynamic viscosity (ISO 80000-4) of the fluid, and is characteristic speed (ISO 80000-3) of the fluid

11-4.29 Pn quotient of power consumption by agitators due to drag and rotational inertial power in fluids, expressed by PnPn / d 35; where P is active power (IEC 80000-6) consumed by a stirrer, ρ is mass density (ISO 80000-4) of fluid, n is rotational frequency (ISO 80000-3), and d is diameter (ISO 80000-3) of stirrer

11-4.30 Richardson Ri quotient of potential energy and kinetic energy for a falling body, In geophysics differences of these quantities are of interest. number expressed by

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No. Name Symbol Definition Remarks

R i g h /v2 ; where g is acceleration of free fall (ISO 80000-3), h is characteristic height (ISO 80000-3), and v is characteristic speed (ISO 80000-3)

11-4.31 Reech number Ree relation between the speed of an object submerged in water relative to the The Reech number can be used to determine the resistance water, and wave propagation speed, expressed by of a partially submerged object (e.g. a ship) of length l (in direction of the motion) moving through water. Ree gl /v ; where A similar quantity is defined as the Boussinesq number g is acceleration of free fall (ISO 80000-3), Bsglv/2 . l is characteristic length (ISO 80000-3), and is speed (ISO 80000-3) of the object relative to the water

11-4.32 Stk quotient of friction and inertia forces for particles in a fluid or in a plasma, In most cases tlr  /v ; where l is characteristic length, and expressed by is speed of fluid. The characteristic length can be the Stktt ra/ ; where diameter of an obstacle or hole.

tr is relaxation time (ISO 80000-12) of particles to achieve fluid’s velocity due to friction (viscosity), and

ta is time (ISO 80000-3) of fluid to alter its velocity under external influence

11-4.33 Stokes number Stk1 quotient of friction and inertia forces for the special case of particles Sometimes the inverse of this number is wrongly used. 2 Stkdf1  / ; where  is kinematic viscosity (ISO 80000-4) of the fluid or plasma, d is diameter (ISO 80000-3) of particle, and f is frequency (ISO 80000-3) of particle vibrations

11-4.34 Stokes number Stk2 Stokes number for calibration of rotameters metering vertical flows of In general use, this value is multiplied by 1,042. ; fluids by means of a floating body, expressed by See also the (item 11-6.12). power coefficient

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No. Name Symbol Definition Remarks

r33 gm   r gm 11 Stk  b   ; where 2 22 bb  r is ratio of pipe and float radii, g is acceleration of free fall (ISO 80000-3), m is mass (ISO 80000-4) of the body, ρ is mass density (ISO 80000-4) of the fluid, η is dynamic viscosity (ISO 80000-4) of the fluid,

ρb is mass density (ISO 80000-4) of the body, and  is kinematic viscosity (ISO 80000-4) of the fluid

11-4.35 Stokes number Stk3 relation between viscous forces and gravity forces for particles falling in a fluid, expressed by 2 Stkgl3 v / ; where v is characteristic speed (ISO 80000-3) of particles, is kinematic viscosity (ISO 80000-4) of the fluid, g is acceleration of free fall (ISO 80000-3), and l is length (ISO 80000-3) of fall

11-4.36 Stokes number Stk4 quotient of drag force and internal friction forces for particles dragged in a fluid

StkFl4D /v ; where

FD is drag force (ISO 80000-4), η is dynamic viscosity (ISO 80000-4), is speed (ISO 80000-3), and l is characteristic length (ISO 80000-3)

11-4.37 ; La, relation between capillary forces and viscous forces when characterizing The Laplace number is also the ratio of surface tension to Suratman Su free surface flow, expressed by momentum transfer, especially dissipation, inside a fluid. number La Su l/ 2 ; where The Laplace number is also given by

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No. Name Symbol Definition Remarks

γ is surface tension (ISO 80000-4), LaSuOhReWe 1// 22 ; where ρ is mass density (ISO 80000-4) of the fluid, Oh is the (item 11-7.4), l is characteristic length (ISO 80000-3), and Re is the Reynolds number (item 11-4.1), and η is dynamic viscosity (ISO 80000-4) of the fluid We is the Weber number (item 11-4.5).

11-4.38 Blake number Bl relation between inertial forces and viscous forces in a porous material, The Blake number can be interpreted as a Reynolds expressed by number for flow in porous material. vl Bl  ; where 1 v is speed (ISO 80000-3) of the fluid, ρ is mass density (ISO 80000-4) of the fluid, l is characteristic length (ISO 80000-3) defined as the volume of a particle divided by its surface area, η is dynamic viscosity (ISO 80000-4) of the fluid, and ε is porosity of the material (=void fraction)

11-4.39 Sommerfeld So, relation between viscous force and load force in a lubrication boundary, Sometimes the inverse of this number is wrongly used. number Sm expressed by 2 nr So ; where pc η is dynamic viscosity (ISO 80000-4) of the lubricant, n is rotational frequency (ISO 80000-3), p is mean bearing pressure (ISO 80000-4), r is radius (ISO 80000-3) of the shaft, and c is radial distance (ISO 80000-3) between rotating shaft and annulus

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No. Name Symbol Definition Remarks

11-4.40 Ta relation between centrifugal force and viscous force of a rotating shaft, Sometimes the square root of this quantity is wrongly used. Ta4/2 l 4 2 ; where annulus is given by 2 3 ω is angular velocity (ISO 80000-3) of rotation, Taraa / ; where l is length (ISO 80000-3) perpendicular to the rotation axis, and ω is angular velocity (ISO 80000-3) of the shaft,  is kinematic viscosity (ISO 80000-4) is kinematic viscosity (ISO 80000-4),

rrr21/2 is mean radius (ISO 80000-3) of the annulus, and

arr 21 is width of the annulus, where

r1 is inner radius of the annulus, and

r2 is outer radius of the annulus. Sometimes the square root of this quantity is used; this use is deprecated.

11-4.41 Ga relation between gravitational force and viscous force in fluid films flowing The Galilei number is also given by over walls, expressed by GaReRi2 or Gagl 32/ ; where Ga Re22/ Fr ; where g is acceleration of free fall (ISO 80000-3), Re is the Reynolds number (item 11-4.1), l is characteristic length (ISO 80000-3), and Ri is the (item 11-4.30), and is kinematic viscosity (ISO 80000-4) of the fluid Fr is the Froude number (item 11-4.3).

11-4.42 Womersley Wo, relation between inertial forces and viscous forces in oscillating flows of The is used for pulsating flows e.g. in number α fluids in pipes, expressed by blood flow. WoR / ; where R is (effective) radius (ISO 80000-3) of the pipe, ω is angular frequency (ISO 80000-3) of oscillations, and is kinematic viscosity (ISO 80000-4)

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5 Transfer of heat

Table 2 gives the names, symbols and definitions of characteristic numbers used to characterize processes in which heat transfer plays a predominant role. Transfer of heat (thermal energy) (ISO 80000-5), occurs either by (convective) transfer of matter with velocity v, or by conduction (diffusion) when a temperature difference exists, or by radiation. Transfer of heat needs a certain time t for a distance d which depends on the velocity v of convection or, in the case of conduction, on material constants like the thermal conductivity λ (ISO 80000-5) or the thermal diffusivity    /  cp (ISO 80000-5), which can depend on other quantities like temperature and pressure. Transfer of energy by radiation is considered to occur instantaneously.

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Table 2 — Characteristic numbers for heat transfer

No. Name Symbol Definition Remarks

11-5.1 Fourier number Fo relation between heat conduction rate and the rate of thermal energy The characteristic length l of the body is often defined as storage in a body for conductive heat transfer into a body, expressed by the quotient of the body’s volume and its heated surface.  t Sometimes the reciprocal of this number is wrongly used. Fo ; where l2 α is thermal diffusivity (ISO 80000-5), t is time (ISO 80000-3), and l is characteristic length (ISO 80000-3)

11-5.2 Péclet number Pe relation between convective heat transfer rate and conductive heat The thermal Péclet number is also given by transfer rate, expressed by PeRePr ; where Pelv / ; where Re is the Reynolds number (item 11-4.1), and v is speed (ISO 80000-3), Pr is the (item 11-7.1). l is length (ISO 80000-3) in the direction of heat transfer, and Compare with item 11-6.2, Péclet number for mass α is thermal diffusivity (ISO 80000-5) transfer.

11-5.3 Rayleigh number Ra relation between buoyancy forces due to thermal expansion and viscous The Rayleigh number is also given by forces in free convection in buoyancy driven flow near a heated surface Ra Gr Pr ; where perpendicular to the gravity force, expressed by Gr is the Grashof number (item 11-4.4), and lgT3   Ra V ; where Pr is the Prandtl number (item 11-7.1).  l is distance (ISO 80000-3) from the wall, g is acceleration of free fall (ISO 80000-3),

αV is cubic expansion coefficient (ISO 80000-5) of the fluid, T is difference of thermodynamic temperature (ISO 80000-5) between surface of the wall and the fluid far away from the wall,  is kinematic viscosity (ISO 80000-4) of the fluid, and α is thermal diffusivity (ISO 80000-5) of the fluid

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No. Name Symbol Definition Remarks

11-5.4 Froude number Fr* quotient of gravitational forces and thermodiffusion forces for heat transfer in of fluids, expressed by gl3 Fr*  ; where 2 g is acceleration of free fall (ISO 80000-3), l is characteristic length (ISO 80000-3), and α is thermal diffusivity (ISO 80000-5)

11-5.5 Nu relation between the internal thermal resistance of a body and its surface The body under consideration can be a solid body, a fluid, thermal resistance in a body transferring heat from a surface into its or their combination, and additional heat transfer due to interior or vice versa, expressed by convective motion can occur. NuK lKlc//  ; where In case of merely conductive heat transfer especially in a p solid body, the “ for heat transfer” (item 11- K is coefficient of heat transfer (ISO 80000-5) through 5.6) is used. the surface, l is length (ISO 80000-3) of the body in direction of heat flow, λ is thermal conductivity (ISO 80000-5) of the surface, α is thermal diffusivity (ISO 80000-5), ρ is mass density (ISO 80000-4), and

cp is specific heat capacity at constant pressure (ISO 80000-5)

11-5.6 Biot number Bi special case of the Nusselt number for heat transfer (item 11-5.5) in case of The characteristic length is commonly defined as the conductive heat transfer in a solid body, expressed by volume of the body divided by its surface area. BiK l / ; where K is coefficient of heat transfer (ISO 80000-5) through the surface, l is characteristic length (ISO 80000-3), and λ is thermal conductivity (ISO 80000-5) of the body

11-5.7 St relation between heat transfer into a fluid from a surface and its heat The Stanton number is also given by transfer by convection, expressed by St Nu// Re  Pr   Nu Pe ; where

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No. Name Symbol Definition Remarks StKc / v ; where Nu is Nusselt number for heat transfer (item p 11-5.5), K is coefficient of heat transfer (ISO 80000-5) through Re is the Reynolds number (item 11-4.1), the surface, Pr is the Prandtl number (item 11-7.1), and ρ is mass density (ISO 80000-4), Pe is the Péclet number (item 11-5.2). is speed (ISO 80000-3), and v Sometimes this quantity is called Margoulis number, cp is specific heat capacity at constant pressure (ISO 80000-5) symbol Ms or Mg. of the fluid

11-5.8 j-factor j, relation between heat transfer and mass transfer in a fluid, expressed by The heat transfer factor is also given by ; Co, 2/3 jStPr2/3 ; where K cp heat transfer j ; where Jq  St is the Stanton number for heat transfer (item factor; cpv  11-5.7), and Colburn number K is coefficient of heat transfer (ISO 80000-5), Pr is the Prandtl number (item 11-7.1). cp is specific heat capacity at constant pressure (ISO 80000-5), See also mass transfer factor (item 11-6.7). ρ is mass density (ISO 80000-4), is speed (ISO 80000-3), η is dynamic viscosity (ISO 80000-4), and λ is thermal conductivity (ISO 80000-5)

11-5.9 Bejan number Be1 quotient of mechanical work and frictional and thermal diffusion energy losses for a forced flow, expressed by pl2 Be  ; where 1  p is drop of pressure (ISO 80000-4) along a pipe, l is length (ISO 80000-3) of the pipe, η is dynamic viscosity (ISO 80000-4), and α is thermal diffusivity (ISO 80000-5)

11-5.10 Bejan number BeS efficiency of heat transfer by a fluid, expressed by

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No. Name Symbol Definition Remarks ST  Be  ; where S S T   S   p  ST  is entropy generation contributed by heat transfer, and Sp  is entropy generation contributed by fluid friction

11-5.11 Stefan number Ste, relation between heat content and latent heat content in a binary mixture StecTQp / ; where

cp is specific heat capacity at constant pressure (ISO 80000-5), T is difference of thermodynamic temperature T (ISO 80000-5) between the phases, and Q is quotient of latent heat of phase transition (ISO 80000-5) and mass (ISO 80000-4)

11-5.12 Brinkman Br, relation between heat produced by viscosity and heat conducted from a

number NBr wall adjacent to a fluid moving relative to it, expressed by BrTv2 / ; where η is dynamic viscosity (ISO 80000-4), v is characteristic speed (ISO 80000-3), λ is thermal conductivity (ISO 80000-5), and

TTTW0 is difference of thermodynamic temperature T (ISO 80000-5), where

T0 is bulk fluid temperature, and

TW is wall temperature

11-5.13 Clausius number Cl relation between energy transfer associated with fluid momentum and energy transfer by thermal conduction in forced heating, expressed by Clv3 l/( T ) ; where is speed (ISO 80000-3), l is length (ISO 80000-3) of the path of energy transfer, 20 DRAFT SAUDI STANDADR SASO ISO 80000-11: 2020

No. Name Symbol Definition Remarks ρ is mass density (ISO 80000-4), λ is thermal conductivity (ISO 80000-5), and T is difference of thermodynamic temperature T (ISO 80000-5) along length l

11-5.14 Carnot number Ca theoretical maximum efficiency (ISO 80000-5) of a Carnot cycle operating between temperature reservoirs

CaTTT 212 / ; where T is thermodynamic temperature (ISO 80000-5), and

T2, T1 are the thermodynamic temperatures of a heat source and a heat sink, respectively

11-5.15 ; Ec relation between the kinetic energy of a flow and its enthalpy change in Dulong number fluid dynamics exhibiting dissipation, expressed by 2 Ecv  cp T  ; where v is characteristic speed (ISO 80000-3),

cp is specific heat capacity at constant pressure (ISO 80000-5) of the flow, and T is difference of thermodynamic temperature T (ISO 80000-5) due to dissipation (by friction)

11-5.16 Gz relation between heat transferred by convection and heat transferred by conduction in a laminar flow in a pipe, expressed by vd2 Gz  ; where l is speed (ISO 80000-3) of the fluid, d is diameter (ISO 80000-3) of the pipe, α is thermal diffusivity (ISO 80000-5) of the fluid, and l is length (ISO 80000-3) of the pipe

11-5.17 heat transfer KQ relation between heat transferred by a flow and its kinetic energy, number expressed by 21 DRAFT SAUDI STANDADR SASO ISO 80000-11: 2020

No. Name Symbol Definition Remarks

32 KlQ /v ; where Φ is heat flow rate (ISO 80000-5), v is characteristic speed (ISO 80000-3), l is characteristic length (ISO 80000-3), and ρ is mass density (ISO 80000-4)

11-5.18 Pomerantsev Po, relation between heat generated in a body and conducted heat in the body, Similar numbers are known for areic, lineic and point number Pov expressed by sources of heat, each with decreasing power of length l 2 respectively. Po Qm l/ T  ; where

Qm is (constant) volumic heat generation rate, l is characteristic length (ISO 80000-3), λ is thermal conductivity (ISO 80000-5), and

TTTm0 is difference of thermodynamic temperature (ISO 80000-5) between that of the medium (Tm) and the initial temperature of the body (T0)

11-5.19 Boltzmann Bz, relation between convective heat and radiant heat for a fluid in a channel, number Bol, expressed by 3 Bo BzcTv p /() ; where ρ is mass density (ISO 80000-4) of the fluid, is characteristic speed (ISO 80000-3) of the fluid,

cp is specific heat capacity at constant pressure (ISO 80000-5), ε is emissivity (ISO 80000-7),  is the Stefan-Boltzmann constant (ISO 80000-7), and T is thermodynamic temperature (ISO 80000-5)

11-5.20 Stark number Sk relation between radiant heat and conductive heat multiplied by the T The relative temperature difference is defined by ; DEPRECATED: relative temperature difference for a body, expressed by T Stefan number 3 Sk T l/  ; where where TTT sl  is the difference of the temperature at the

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No. Name Symbol Definition Remarks

DEPRECATED: ε is emissivity (ISO 80000-7) of the surface, surface, Ts, and the temperature at a layer at a distance l Biot radiation  is the Stefan-Boltzmann constant (ISO 80000-7), from the surface, Tl. number T is thermodynamic temperature (ISO 80000-5), Sometimes this characteristic number is wrongly defined without the factor ε. l is characteristic length (ISO 80000-3), and λ is thermal conductivity (ISO 80000-5)

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6 Transfer of matter in a binary mixture

Table 3 gives the names, symbols and definitions of characteristic numbers used to characterize processes in which transfer of matter in a binary mixture plays a predominant role. Transfer of matter in a binary mixture is accomplished in general by diffusion with its coefficient D (ISO 80000-9). The two components can move with speed v relative to each other, and the movement of one component can be influenced by the other one.

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Table 3 — Characteristic numbers for transfer of matter in a binary mixture

No. Name Symbol Definition Remarks

11-6.1 Fourier number Fo* relation between diffusive mass transfer within a given duration and mass The Fourier number for mass transfer is also given by storage rate in transient mass transfer, expressed by FoFoLe*  / ; where Dt Fo*  ; where Fo is the Fourier number for heat transfer 2 l (item 11-5.1), and D is diffusion coefficient (ISO 80000-9), Le is the (item 11-7.3). t is duration (ISO 80000-3) of observation, and See also the Fourier number for heat transfer (item 11-5.1). l is length (ISO 80000-3) of transfer

11-6.2 Péclet number Pe* , relation between advective mass transfer rate and longitudinal diffusive The Péclet number for mass transfer is also given by ; mass transfer rate for mass transfer in reactors, expressed by Bd, PePeLeReSc*  ; where Bodenstein * Bod PelDv / ; where Pe is the Péclet number for heat transfer, number v is speed (ISO 80000-3), Le is the Lewis number (item 11-7.3), l is characteristic length (ISO 80000-3), and Re is the Reynolds number (item 11-4.1), and D is diffusion coefficient (ISO 80000-9) Sc is the Schmidt number (item 11-7.2). Compare with item 11-5.2, the Péclet number for heat transfer.

11-6.3 Grashof number Gr* relation between buoyancy forces and viscous forces in natural convection Instead of “amount-of-substance fraction” the “amount-of- of fluids, expressed by substance concentration” (ISO 80000-9) is used also. Grlgx*32/ ; where Compare with item 11-4.4, the Grashof number. l is characteristic length (ISO 80000-3), g is acceleration of free fall (ISO 80000-3),

1/     / x Tp, , where ρ is mass density (ISO 80000-4) of the fluid, and x is amount-of-substance fraction (ISO 80000-9), x is difference of amount-of-substance fraction (ISO 80000-9) along length l, and

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No. Name Symbol Definition Remarks  is kinematic viscosity (ISO 80000-4)

11-6.4 Nusselt number Nu* relation between mass flux at an interface and specific flux by pure Sometimes this quantity is called the , Sh. molecular diffusion in a layer of thickness l for mass transfer at the Compare with item 11-5.5, Nusselt number for heat boundary of a fluid, expressed by transfer. NuklD* / ; where

k’ is mass flux density qAm / through the surface, where

qm is mass flow rate (ISO 80000-4), and A is area (ISO 80000-3), l is thickness (ISO 80000-3), ρ is mass density (ISO 80000-4) of the fluid, and D is diffusion coefficient (ISO 80000-9)

11-6.5 Stanton number St* relation between mass transfer perpendicular to the surface of a fluid flow The Stanton number for mass transfer is also given by and mass transfer parallel to the surface in a free surface flow, expressed StNuPe*** / ; where by Nu* is the Nusselt number for mass transfer Stk* /v ; where (item 11-6.4), and k’ is mass flux density through the surface, where qAm / Pe* is the Péclet number for mass transfer

qm is mass flow rate (ISO 80000-4), and (item 11-6.2). A is area (ISO 80000-3), Compare with item 11-5.7, the Stanton number for heat ρ is mass density (ISO 80000-4), and transfer. v is speed (ISO 80000-3)

11-6.6 Graetz number Gz* quotient of advective mass transfer rate and radial diffusive mass transfer rate for mass transfer in pipes, expressed by vdd Gz** Pe ; where Dl is characteristic speed (ISO 80000-3) of the fluid, d is hydraulic diameter (ISO 80000-3) of the pipe, D is diffusion coefficient (ISO 80000-9),

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No. Name Symbol Definition Remarks l is length (ISO 80000-3) of the pipe, and Pe* is the Péclet number for mass transfer (item 11-6.2)

11-6.7 mass transfer j* relation between mass transfer perpendicular to the surface of a fluid and The mass transfer factor is also given by factor; mass transfer parallel to the surface in an open flow of fluids, expressed by **2/3 jjStScm  ; where j-factor 2/3 * k  j   ; where St* is the Stanton number for mass transfer v D (item 11-6.5), and k is the mass transfer coefficient through the surface, Sc is the Schmidt number (item 11-7.2). kk/ , where See also heat transfer factor (item 11-5.17). ρ is mass density (ISO 80000-4),

k’ is mass flux density qAm / through the surface, where

qm is mass flow rate (ISO 80000-4), and A is area (ISO 80000-3), v is speed (ISO 80000-3),  is kinematic viscosity (ISO 80000-4), and D is diffusion coefficient (ISO 80000-9)

11-6.8 At scaled density difference of heavier and lighter fluids, expressed by The Atwood number is used in the study of hydrodynamic  instabilities in density stratified flows. At  12; where 12

ρ1 is density of heavier fluid, and

ρ2 is density of lighter fluid

11-6.9 Biot number Bi* relation between mass transfer rate at the interface and mass transfer rate in the interior of a body, expressed by * Bi kl/ Dint ; where k is the mass transfer coefficient through the surface, kk/ , where ρ is mass density (ISO 80000-4),

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No. Name Symbol Definition Remarks

k’ is mass flux density qAm / through the surface, where

qm is mass flow rate (ISO 80000-4), and A is area (ISO 80000-3), l is thickness (ISO 80000-3) of layer, and

Dint is diffusion coefficient (ISO 80000-9) at the interface

11-6.10 Mo quotient of gravitational forces and viscous forces for gas bubbles in a The Morton number is used to determine the shape of liquid, or liquid drops in a gas, expressed by bubbles or drops. 4 g b The Morton number is also given by Mo1 ; where  3  MoWeFrRe 324 ; where g is acceleration of free fall (ISO 80000-3), We is the Weber number (item 11-4.5), η is dynamic viscosity (ISO 80000-4) of the surrounding fluid, Fr is the Froude number (item 11-4.3), and ρ is mass density (ISO 80000-4) of the surrounding fluid, Re is the Reynolds number (item 11-4.1). γ is surface tension (ISO 80000-4) of the interface, and

ρb is mass density (ISO 80000-4) of the bubble or drop

11-6.11 Bond number; Bo, quotient of inertial force and capillary force for gas bubbles or liquid drops In the case of gravity a = g acceleration of free fall Eötvös number Eo in a fluid, expressed by (ISO 80000-3), the name Eötvös number is mostly used.  The Bond number is also given by a 2 b Bol 1 ; where  BoWeFr / ; where a is the acceleration of the body (ISO 80000-3), mostly We is the Weber number (item 11-4.5), and acceleration of free fall, g (ISO 80000-3), Fr is the Froude number (item11-4.3). γ is surface tension (ISO 80000-4) of the interface, The Bond number is also used for driven by ρ is density (ISO 80000-4) of the medium, buoyancy. l is characteristic length (ISO 80000-3) (radius of a drop or radius of a capillary tube), and

ρb is mass density (ISO 80000-4) of the drop or bubble

11-6.12 Archimedes Ar quotient of buoyancy forces and viscous forces in fluids motion due to In this definition, the body can be replaced by an immiscible number density differences for a body in a fluid, expressed by fluid. See also Stokes number (item 11-4.34). 28 DRAFT SAUDI STANDADR SASO ISO 80000-11: 2020

No. Name Symbol Definition Remarks

3 gl b Ar 1 ; where  2  g is acceleration of free fall (ISO 80000-3), l is characteristic length (ISO 80000-3) of the body,  is kinematic viscosity (ISO 80000-4) of the fluid,

ρb is mass density (ISO 80000-4) of the body, and ρ is mass density (ISO 80000-4) of the fluid

11-6.13 expansion Ex quotient of buoyancy force and inertial force in moving fluids due to number density differences for gas bubbles rising in a liquid, expressed by

gd b Ex 1 ; where v2  g is acceleration of free fall (ISO 80000-3), d is diameter (ISO 80000-3) of bubbles, v is speed (ISO 80000-3) of bubbles,

ρb is mass density (ISO 80000-4) of bubbles, and ρ is mass density (ISO 80000-4) of the liquid

11-6.14 Marangoni Mg, quotient of heat transferred by Marangoni convection and heat transferred The Marangoni convection is free surface flow due to number Mar by thermal diffusivity in thermo-capillary convection of liquid films on a different surface tensions caused by a temperature free surface, expressed by gradient. T d This quantity is sometimes called Thompson number. Mgl ; where aTd l is characteristic thickness (ISO 80000-3) of the film, T is difference of thermodynamic temperature T (ISO 80000-5) between surface and outer surface of the film, η is dynamic viscosity (ISO 80000-4) of the liquid, a is thermal diffusivity (ISO 80000-5) of the liquid, and γ is surface tension (ISO 80000-4) of the film

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No. Name Symbol Definition Remarks

11-6.15 Lockhart- Lp quotient of mass flow rates multiplied by the square root of density in a The Lockhart-Martinelli parameter is used, for example, in Martinelli two-phase flow, expressed by boiling or condensing. parameter m g Lp l ; where mgl

mqlm is liquid phase mass flow rate (ISO 80000-4),

mg is gas phase mass flow rate,

ρg is gas density (ISO 80000-4), and

ρl is liquid density

11-6.16 Bejan number Be* , quotient of mechanical work and frictional and diffusion energy loss in A similar quantity exists for heat transfer (item 11-5.9). viscous flow of fluids in pipes, expressed by Be2 pl2 Be*  ; where  D p is drop of pressure (ISO 80000-4) along a pipe or channel, l is length (ISO 80000-3) of channel, η is dynamic viscosity (ISO 80000-4) of the fluid, and D is diffusion coefficient (ISO 80000-9), mass diffusivity

11-6.17 Ca, quotient of the excess of local static head over vapour pressure head and The cavitation number represents the ratio of the excess of number Cn velocity head for fast flow in liquids, expressed by local static head over vapour pressure head to velocity pp head. Ca v ; where v2 /2 p is local static pressure (ISO 80000-4),

pv is vapour pressure (ISO 80000-4) of the fluid, ρ is mass density (ISO 80000-4) of the fluid, and v is characteristic speed (ISO 80000-3) of the flow

11-6.18 absorption Ab relation between mass flow rate and surface area for gas absorption at number wetted walls, expressed by

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No. Name Symbol Definition Remarks

ld Ab k ; where DqV k is the mass transfer coefficient through the surface, kk '/ , where ρ is mass density (ISO 80000-4), and

k’ is mass flux density through the surface, k’ = qm/A, where

qm is mass flow rate (ISO 80000-4), and A is area (ISO 80000-3), l is length (ISO 80000-3) of wetted surface, d is thickness (ISO 80000-3) of liquid film, D is diffusion coefficient (ISO 80000-9), and

qV is volume flow rate (ISO 80000-4) per wetted perimeter

11-6.19 Ca quotient of gravitational forces and capillary forces for fluids in narrow pipes, expressed by Cadg 2/ ; where d is diameter (ISO 80000-3) of the pipe, ρ is mass density (ISO 80000-4) of the fluid, g is acceleration of free fall (ISO 80000-3), and γ is surface tension (ISO 80000-4) of the fluid

11-6.20 dynamic capillary Ca* , quotient of viscous force and capillary force acting across an interface The dynamic capillary number is also given by the quotient number between a liquid and a gas, or between two immiscible liquids for a flow of of the Weber number and the Reynolds number. Cn fluid influenced by interfacial tension, expressed by Ca* v/ ; where η is dynamic viscosity (ISO 80000-4) of the fluid, v is characteristic speed (ISO 80000-3), and γ is surface or interfacial tension (ISO 80000-4)

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7 Constants of matter

Table 4 gives the names, symbols and definitions of some constants of matter, concerning mechanic, electric and thermodynamic properties of material, as well as their relationships. Some of the most widely known are not listed in the table because they are given in other parts of the ISO 80000 series, e.g. the ratio of the specific heat capacities, γ (ISO 80000-5), or the emissivity, ε (ISO 80000-7).

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Table 4 — Constants of matter

No. Name Symbol Definition Remarks

11-7.1 Prandtl number Pr quotient of kinematic viscosity and thermal diffusivity for a fluid, The Prandtl number also represents the quotient of heat expressed by produced by viscosity and heat transferred by thermal Pra / ; where diffusivity. The mass transfer analogue of the Prandtl number is the  is kinematic viscosity (ISO 80000-4), and Schmidt number (item 11-7.2). a is thermal diffusivity (ISO 80000-5) The Prandtl number is also given by Pr = Pe/Re; where Pe is the Péclet number (item 11-5.2), and Re is the Reynolds number (item 11-4.1).

11-7.2 Schmidt number Sc quotient of kinematic viscosity and diffusion coefficient for a fluid, The heat transfer analogue of the Schmidt number is the DEPRECATED: expressed by Prandtl number (item 11-7.1). Colburn number ScD / ; where is kinematic viscosity (ISO 80000-4), and D is diffusion coefficient (ISO 80000-9)

11-7.3 Lewis number Le quotient of thermal diffusivity and diffusion coefficient for heat transfer in The Lewis number is also given by a fluid, expressed by Le Sc/ Pr ; where LeaD / ; where Sc is the Schmidt number (item 11-7.2), and a is thermal diffusivity (ISO 80000-5), and Pr is the Prandtl number (item 11-7.1). D is diffusion coefficient (ISO 80000-9) Compare with item 11-5.2. The Lewis number is sometimes defined as reciprocal of this quantity.

11-7.4 Ohnesorge Oh relation between viscous force and the square root of the product of inertia The Ohnesorge number is also given by number force and capillary force for atomization of liquids, expressed by Oh We/ Re ; where  Oh ; where We is the Weber number (item 11-4.5), and l Re is the Reynolds number (item 11-4.1).

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No. Name Symbol Definition Remarks η is dynamic viscosity (ISO 80000-4), See also Laplace number (item 11-4.37). γ is surface tension (ISO 80000-4), The characteristic length typically is the drop diameter. ρ is mass density (ISO 80000-4), and l is characteristic length (ISO 80000-3)

11-7.5 ; Cy relation between inertia forces and compression forces in compressible aeroelasticity fluids, expressed by parameter Cyv2 / K ; where ρ is mass density (ISO 80000-4), v is speed (ISO 80000-3), and K is modulus of compression, bulk modulus (ISO 80000-4)

11-7.6 Hooke number Ho2 relation between inertia forces and linear stress forces in elastic fluids, expressed by 2 HoE2 v / ; where ρ is mass density (ISO 80000-4), is speed (ISO 80000-3), and E is modulus of elasticity (ISO 80000-4)

11-7.7 Weissenberg Wi product of time derivative of shear rate and relaxation time in viscoelastic The represents the relative number flows, expressed by importance of viscous forces when compared to elastic forces. Wit r ; where The time derivative of shear strain is sometimes called the  is time derivative of shear strain (ISO 80000-4), and shear rate. tr is relaxation time (ISO 80000-12)

11-7.8 Deborah number De quotient of relaxation time of viscoelastic fluids and observation duration The stress relaxation time is sometimes called the Maxwell in rheology of viscoelastic fluids, expressed by relaxation time.

De tcp/ t ; where

tc is stress relaxation time, and

tp is observation duration (ISO 80000-3)

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No. Name Symbol Definition Remarks

11-7.9 Lorentz number Lo quotient of electrical conductivity and thermal conductivity, expressed by  U 2 Lo ; where T  is electrical conductivity (IEC 80000-6), U is difference of voltage U (ISO 80000-6) between two reference points, λ is thermal conductivity (ISO 80000-5), and T is difference in thermodynamic temperature T (ISO 80000-5) between the reference points

11-7.10 compressibility Z quotient of isothermal compressibility (ISO 80000-5) of a gas and that of number an ideal gas, expressed by p Z  ; where RTS

p is pressure (ISO 80000-4), ρ is mass density (ISO 80000-4),

Rs is specific gas constant (ISO 80000-5), and T is thermodynamic temperature (ISO 80000-5)

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8

Table 5 gives the names, symbols and definitions of characteristic numbers found in magnetohydrodynamics (MHD). MHD is concerned with the dynamics of electrically conducting fluids, which are characterized by material constants such as mass density (ISO 80000-4), magnetic permeability (IEC 80000-6) and electrical conductivity (IEC 80000-6), and which interact with external fields like magnetic flux density (IEC 80000-6).

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Table 5 — Characteristic numbers in magnetohydrodynamics

No. Name Symbol Definition Remarks 11-8.1 Reynolds Rm relation between inertial force and magneto-dynamic viscous force in an This number is also called . magnetic electrically conducting fluid, expressed by The Reynolds magnetic number is also given by number Rmllvv / ; where m RmRePrm ; where v is speed (ISO 80000-3) of the fluid, Re is the Reynolds number (item 11-4.1), and

l is characteristic length (ISO 80000-3), Prm is the Prandtl magnetic number (item 11-8.10). μ is magnetic permeability (IEC 80000-6),  is electrical conductivity (IEC 80000-6), and

m 1/ is magnetic viscosity (magnetic diffusivity) 11-8.2 Batchelor Bt relation between inertia and magneto-dynamic diffusion in an electrically number conducting liquid, expressed by

Btlv  / rr; where is speed (ISO 80000-3), l is characteristic length (ISO 80000-3),  is electrical conductivity (IEC 80000-6), μ is magnetic permeability (IEC 80000-6),

εr is relative permittivity (IEC 80000-6), and

μr is relative permeability (IEC 80000-6) 11-8.3 Nusselt electric Ne relation between convective current and diffusive current of ions in This number is also called electric Nusselt number. number electrochemistry, expressed by Sometimes this quantity is called the Reynolds electric Nev l/ D* ; where number. is speed (ISO 80000-3), l is characteristic length (ISO 80000-3), and DDD*  /2 ; where DD, are diffusion coefficients (ISO 80000-9) of positive or negative ions respectively

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No. Name Symbol Definition Remarks 11-8.4 Alfvén number; Al relation between speed of a plasma and the Alfvén wave speed, expressed Often, the inverse of this number is wrongly used. Mach magnetic by The name “Alfvén Mach number” is used in investigations number; v on the solar wind. Al ; where Kárman number B/  The quantity vA B/  is called Alfvén wave speed, v is speed (ISO 80000-3), where B is magnetic flux density (IEC 80000-6), B is magnetic flux density (IEC 80000-6), ρ is mass density (ISO 80000-4), and ρ is mass density (ISO 80000-4), and μ is magnetic permeability (IEC 80000-6) μ is magnetic permeability (IEC 80000-6).

11-8.5 Hartmann Ha relation between magnetically induced stress and hydrodynamic shear The Hartmann number represents also the ratio of number stress in an electrically conducting fluid, expressed by magnetic force to viscous force. HaBl / ; where B is magnetic flux density (IEC 80000-6), l is characteristic length (ISO 80000-3),  is electrical conductivity (IEC 80000-6), and η is dynamic viscosity (ISO 80000-4) 11-8.6 Cowling number Co quotient of magnetic and kinematic energy density in a plasma, expressed The Cowling number also represents the ratio of magnetic ; by to dynamic pressure. Euler magnetic CoB 22/v ; where This quantity is equal to the square of the inverse of the number Alfvén number. B is magnetic flux density (IEC 80000-6), This quantity is often called the Cowling number, μ is magnetic permeability (IEC 80000-6), Co2. ρ is mass density (ISO 80000-4), and The first Cowling number is then defined as CoCo1  Rm ; is speed (ISO 80000-3) where Rm is the Reynolds magnetic number (item 11-8.1). 11-8.7 Stuart electrical Se quotient of electric energy density and kinematic energy density in a The Stuart electrical number is the electrical counterpart number plasma, expressed by of the Cowling number (item 11-8.6). Se E22/v  ; where ε is electric permittivity (IEC 80000-6),

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No. Name Symbol Definition Remarks E is electric field strength (IEC 80000-6), ρ is mass density (ISO 80000-4), and v is speed (ISO 80000-3)

11-8.8 magnetic Nmp quotient of gas pressure and magnetic pressure in a gas or plasma, The quantity pB 2 /2  is called magnetic pressure, pressure number expressed by m where 2 Np ; where B is magnetic flux density (IEC 80000-6), and mp B2 μ is magnetic permeability (IEC 80000-6). p is pressure (ISO 80000-4), μ is magnetic permeability (IEC 80000-6), and B is magnetic flux density (IEC 80000-6)

11-8.9 Chandrasekhar Q, quotient of Lorentz force and viscous force in magnetic convection in a The is also given by Q H a 2 where number Ch fluid, expressed by Ha is the Hartmann number (item 11-8.5). 2 QBl / ; where B is magnetic flux density (IEC 80000-6), l is characteristic length (ISO 80000-3), a length scale of the system,  is electrical conductivity (IEC 80000-6), ρ is mass density (ISO 80000-4), and  is kinematic viscosity (ISO 80000-4)

11-8.10 Prandtl magnetic Prm quotient of kinematic viscosity and magnetic viscosity in an electrically The quantity m 1/ is called magnetic viscosity or number conducting liquid, expressed by magnetic diffusivity. See item 11-8.11. Prm   ; where The Prandtl magnetic number is also given by is kinematic viscosity (ISO 80000-4), PrRmRem  / ; where  is electrical conductivity (IEC 80000-6), and Rm is the Reynolds magnetic number (item μ is magnetic permeability (IEC 80000-6) 11-8.1), and Re is the Reynolds number (item 11-4.1). This number is also called .

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No. Name Symbol Definition Remarks 11-8.11 Roberts number Ro quotient of thermal diffusivity and magnetic viscosity in an electrically The quantity m 1/   is called magnetic viscosity or conducting liquid, expressed by magnetic diffusivity; where Ro ; where μ is magnetic permeability (IEC 80000-6), and α is thermal diffusivity (ISO 80000-5), σ is electrical conductivity (IEC 80000-6).  is electrical conductivity (IEC 80000-6), and μ is magnetic permeability (IEC 80000-6) 11-8.12 Stw quotient of magnetic forces and inertia forces in an electrically conducting The Stuart number sometimes is called magnetic force liquid, expressed by parameter. StwBl 2 /v ; where Sometimes the square root is wrongly used. B is magnetic flux density (IEC 80000-6), The Stuart number is also given by 2 l is characteristic length (ISO 80000-3), StwHaRe / ; where  is electrical conductivity (IEC 80000-6), Ha is the Hartmann number, and v is characteristic speed (ISO 80000-3), and Re is the Reynolds number. ρ is mass density (ISO 80000-4)

11-8.13 magnetic Nmg quotient of magnetic forces and viscous forces in an electrically number conducting fluid, expressed by

NBlmg  /()v ; where B is magnetic flux density (IEC 80000-6), l is characteristic length (ISO 80000-3),  is electrical conductivity (IEC 80000-6), η is dynamic viscosity (ISO 80000-4), and is speed (ISO 80000-3) 11-8.14 electric field Ef quotient of Coulomb force and Lorentz force on moving electrically parameter charged material or particles, expressed by EfEB /v ; where E is electric field strength (IEC 80000-6), is speed (ISO 80000-3), and B is magnetic flux density (IEC 80000-6) 40 DRAFT SAUDI STANDADR SASO ISO 80000-11: 2020

No. Name Symbol Definition Remarks

11-8.15 Hall number Hc, quotient of gyro frequency and collision frequency in a plasma, expressed Sometimes the inverse of this number is wrongly used.

CH by 2π times this quantity is called the Hall parameter.   H  c ; where c 2 v

ωc is cyclotron angular frequency (ISO 80000-10), λ is mean free path (ISO 80000-9), and v is average speed (ISO 80000-3)

11-8.16 Lundquist Lu quotient of Alfvén speed and magneto-dynamic speed in a plasma, The quantity v B/  is called Alfvén wave speed. See number expressed by A item 11-8.4.  LuBl  ; where The quantity v 1/l is called magneto dynamic  m speed; where B is magnetic flux density (IEC 80000-6), l is characteristic length (ISO 80000-3), l is characteristic length (ISO 80000-3),  is electrical conductivity (IEC 80000-6), and  is electrical conductivity (IEC 80000-6), μ is magnetic permeability (IEC 80000-6). μ is magnetic permeability (IEC 80000-6), and The Lundquist number is also given by ρ is mass density (ISO 80000-4) LuRmAl / ; where Rm is the Reynolds magnetic number (item 11-8.1), and Al is the Alfvén number (item 11-8.4). See also Hartmann number (item 11-8.5).

11-8.17 magnetic Jom quotient of Joule heating energy and magnetic field energy in a plasma, This number is also called magnetic Joule number. number expressed by 2 JocTBm 2/ p ; where ρ is mass density (ISO 80000-4), μ is magnetic permeability (IEC 80000-6),

cp is specific heat capacity at constant pressure (ISO 80000-5), T is thermodynamic temperature (ISO 80000-5), and B is magnetic flux density (IEC 80000-6)

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No. Name Symbol Definition Remarks

11-8.18 Grashof Grm mathematical expression for the heat transfer by free thermo-magnetic This number is also called magnetic Grashof number. magnetic convection of a paramagnetic fluid under gravity, See also Grashof number (item 11-4.4). number 3 GrgTlvmee4/ V ; where

e is electrical conductivity (IEC 80000-6),

μe is magnetic permeability (IEC 80000-6), g is acceleration of free fall (ISO 80000-3),

αV is cubic expansion coefficient (ISO 80000-5),

TTTS  is difference of thermodynamic temperature T (ISO 80000-5), where TS is surface temperature and T∞ is bulk temperature l is characteristic length (ISO 80000-3), and  is kinematic viscosity (ISO 80000-4)

11-8.19 Naze number Na quotient of velocity of Alfvén waves and velocity of sound in a plasma, The quantity v B/  is called Alfvén wave speed. See expressed by A item 11-8.4. NaBc /  ; where B is magnetic flux density (IEC 80000-6), c is speed of sound (ISO 80000-8), ρ is mass density (ISO 80000-4), and μ is magnetic permeability (IEC 80000-6)

11-8.20 Reynolds electric Ree quotient of speed of a fluid and average drift speed of the charged This number is also called electrical Reynolds number. number particles in an electrically conducting fluid, expressed by The drift speed of the charged particles in an electric field

Releeev/ ; where 1 is given by vd  , where v is characteristic speed (ISO 80000-3) of the fluid, E

εe is electric permittivity (IEC 80000-6), E is electric field strength (IEC 80000-6), and

ρe is electric charge density (IEC 80000-6), μ is mobility (ISO 80000-10) of charge carriers. l is characteristic length (ISO 80000-3), and μ is mobility (ISO 80000-10) of charge carriers

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No. Name Symbol Definition Remarks 11-8.21 Ampère number Am relation between electric surface current and magnetic field strength in an This number is also called magnetic field number. electrically conducting liquid, expressed by The electric surface current is given by AmIlH / ; where A IlEAA; where

IA is electric surface current, ρA is surface density of electric charge l is characteristic length (ISO 80000-3), and (IEC 80000-6), H is magnetic field strength (IEC 80000-6) l is characteristic length (ISO 80000-3), µ is mobility (ISO 80000-10) of charge carriers, and E is electric field strength (IEC 80000-6).

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9 Miscellaneous

Table 6 gives the names, symbols and definitions of characteristic numbers not covered in the previous sections.

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Table 6 — Arrhenius number and Landau-Ginzburg number

No. Name Symbol Definition Remarks 11-9.1 Arrhenius α quotient of chemical activation energy and thermal energy; in a chemical number reaction it is the exponential factor of the reaction rate constant, k, expressed by

k exp , with  ERT0 / ; where

E0 is activation energy (ISO 80000-5), R is molar gas constant (ISO 80000-9), and T is thermodynamic temperature (ISO 80000-5) 11-9.2 Landau-Ginzburg  quotient of penetration depth of a magnetic field into a superconductor number and the coherence length of thermodynamic fluctuations within a superconducting phase in a material at zero thermodynamic temperature, expressed by

 L /2  ; where

λL is London penetration depth (ISO 80000-12), and  is coherence length (ISO 80000-12)

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Bibliography

[1] ISO 80000-3, Quantities and units — Part 3: Space and time

[2] ISO 80000-4, Quantities and units — Part 4: Mechanics

[3] ISO 80000-5, Quantities and units — Part 5:

[4] IEC 80000-6, Quantities and units — Part 6: Electromagnetism

[5] ISO 80000-9, Quantities and units — Part 9: Physical chemistry and molecular physics

[6] ISO 80000-12, Quantities and units — Part 12: Condensed matter physics

[7] CRC Handbook of Chemistry and Physics (ed. Robert C. Weast), 56th Edition, 1975-1976, CRC- Press, Cleveland Ohio

[8] CRC Handbook of Chemistry and Physics (ed. David R. Lide), 88th Edition, 2007-2008, CRC-Press, Boca Raton

[9] HALL, C. W.: Laws and Models: Science, Engineering, and Technology. CRC Press, 28.09.1999; (e- Book)

[10] KUNEŠ, J.: Dimensionless physical quantities in science and engineering. Elsevier 2012, 1st ed (e- book)

[11] MASSEY, B.S.: Units, dimensional analysis and physical similarity. London: Van Nostrand Reinhold Company, 1971

[12] Plasma Formulary, N.R.L., 2013 (ed. J.D. Hubs) Naval Research Laboratory; Washington DC 20375 Printout available from http://wwwppd.=NRL.navy.mil/=NRLformulary/

[13] WETZLER, H.: Kennzahlen der Verfahrenstechnik (in German), Hüthig 1985

[14] WHITE, F. M. Fluid Mechanics, 3rd edition, McGraw-Hill

[15] http://thermopedia.com/

[16] http://www.processassociates.com/process/dimen/dn_all.htm [17] http://goldbook.iupac.org/index.htmlDRAFT

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Alphabetical index

Name Item absorption number 11-6.18 aeroelasticity parameter 11-7.5 Alfvén number 11-8.4 Ampère number 11-8.21 Archimedes number 11-6.12 Arrhenius number 11-9.1 Atwood number 11-6.8 Bagnold number 11-4.10 Bagnold number 11-4.11 Batchelor number 11-8.2 Bejan number 11-4.15 Bejan number 11-5.10 Bejan number 11-5.9 Bejan number 11-6.16 Bingham number 11-4.17 Biot number 11-5.6 Biot number 11-6.9 Blake number 11-4.38 Bodenstein number 11-4.19 Bodenstein number 11-6.2 Boltzmann number 11-5.19 Bond number 11-6.11 11-5.12 capillary number 11-6.19 Carnot number 11-5.14 Cauchy number 11-7.5 cavitation number 11-6.17 Chandrasekhar number 11-8.9 Clausius number 11-5.13 Colburn DRAFTnumber 11-5.8 compressibility number 11-7.10 Cowling number 11-8.6

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Darcy friction factor 11-4.23 Dean number 11-4.14 Deborah number 11-7.8 drag coefficient 11-4.9 Dulong number 11-5.15 dynamic capillary number 11-6.20 Eckert number 11-5.15 Eötvös number 11-6.11 Ekman number 11-4.21 elasticity number 11-4.22 electric field parameter 11-8.14 Euler magnetic number 11-8.6 Euler number 11-4.2 expansion number 11-6.13 Fanning number 11-4.24 Fourier number 11-5.1 Fourier number 11-6.1 Froude number 11-4.3 Froude number 11-5.4 Galilei number 11-4.41 Goertler number 11-4.25 Goertler parameter 11-4.25 Graetz number 11-5.16 Graetz number 11-6.3 Hagen number 11-4.26 Hall number 11-8.15 Hartmann number 11-8.5 heat transfer factor 11-5.8 heat transfer number 11-5.17 Hedström number 11-4.18 Hooke number DRAFT11-7.6 j-factor 11-5.8 j-factor 11-6.7

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Joule magnetic number 11-8.17 Kárman number 11-8.4 Kiebel number 11-4.20 Knudsen number 11-4.7 Lagrange number 11-4.16 Landau-Ginzburg number 11-9.2 Laplace number 11-4.37 Laval number 11-4.27 Lewis number 11-7.3 lift coefficient 11-4.12 Lockhart-Martinelli parameter 11-6.15 Lorentz number 11-7.9 Lundquist number 11-8.16 Mach magnetic number 11-8.4 Mach number 11-4.6 magnetic field number 11-8.21 magnetic number 11-8.13 magnetic pressure number 11-8.8 11-6.14 mass transfer factor 11-6.7 Moody friction factor 11-4.23 Morton number 11-6.10 Naze number 11-8.19 Nusselt electric number 11-8.3 Nusselt number 11-5.5 Nusselt number 11-6.4 Ohnesorge number 11-7.4 Péclet number 11-5.2 Péclet number 11-6.2 plasticity number 11-4.17 Poiseuille number 11-4.28 Pomerantsev number 11-5.18 power coefficient 11-4.34 power numberDRAFT 11-4.29 Prandtl magnetic number 11-8.10 Prandtl number 11-7.1

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Rayleigh number 11-5.3 Reech number 11-4.31 Reynolds electric number 11-8.20 Reynolds magnetic number 11-8.1 Reynolds number 11-4.1 Richardson number 11-4.30 Roberts number 11-8.11 Rossby number 11-4.20 Schmidt number 11-7.2 Sommerfeld number 11-4.39 Stanton number 11-5.7 Stanton number 11-6.5 Stark number 11-5.20 Stefan number 11-5.11 Stokes number 11-4.36 Stokes number 11-4.35 Stokes number ; 11-4.34 Stokes number

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