Assessment of Tire Features for Modeling Vehicle Stability in Case of Vertical Road Excitation
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JAN 30 1968 Efgineering Llbf
\NT O ECJW .' J IS1 1967 4-1P-RA RIE-: OPTIMIZATION OF THE RANDOM VIBRATION CHARACTERISTICS OF VEHICLE SUSPENSIONS by ERICH KENNETH BENDER S.B., Massachusetts Institute of Technology (1962) S.M., Massachusetts Institute of Technology (1963) M.E., Massachusetts Institute of Technology (1966) SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF SCIENCE at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY June, 1967 Signature of Author ., Department of Mechanical Engineering, ') /) Wfril 27, 1967 Certified by Thesfs Su4'sor, /K/J Accepted by ....... ...... Chairman, Departktnital'Commit 4 'ee on Graduate Students .\ST. OF TECHN 010 JAN 30 1968 EfGINEERING Llbf. OPTIMIZATION OF THE RANDOM VIBRATION CHARACTERISTICS OF VEHICLE SUSPENSIONS by ERICH KENNETH BENDER Submitted in partial fulfillment of the require- ments for the degree of Doctor of Science at the Massachusetts Institute of Technology, June, 1967. ABSTRACT Some of the fundamental limitations and trade-offs regard- ing the capabilities of vehicle suspensions to control random vi- brations are investigated. The vehicle inputs considered are sta- tistically described roadway elevations and static loading vara- tions on the sprung mass. The vehicle is modeled as a two-degree- of-freedom linear system consisting of a sprung mass, suspension and an unsprung mass which is connected to the roadway by a spring. The criterion used to optimize the suspension characteristics is the weighted sum of rms vehicle acceleration and clearance space required for sprung mass-unsprung mass relative excursions. Two ap- proaches to find the suspension characteristics which optimize the trade-off between vibration and clearance space are considered. The first, based on Wiener filter theory, is used to synthesize the optimum suspension transfer function. -
Longitudinal & Lateral Directional Short Course
1 Longitudinal & Lateral Directional Short Course Flight One – Effects of longitudinal stability and control characteristics on handling qualities Background: In this flight training exercise we will examine how longitudinal handling qualities are affected by three important variables that are inherent in a given aircraft design. They are: Static longitudinal stability Dynamic longitudinal stability Elevator control effectiveness As you will recall from your classroom briefings, longitudinal stability is responsible for the frequency response to a disturbance, which can be caused by the atmosphere or an elevator control input. It may be described by two longitudinal oscillatory modes of motion: A Long term response (Phugoid), which is a slow or low frequency oscillation, occurring at a relatively constant angle of attack with altitude and speed variations. This response largely affects the ability to trim for a steady state flight condition. A short term response where a higher frequency oscillation occurs at a relatively constant speed and altitude, but with a change in angle of attack. This response is associated with maneuvering the aircraft to accomplish a closed loop task, such as an instrument approach procedure. If static stability is positive; The long and short period responses will either be convergent or neutral (oscillations) depending on dynamic stability If neutral; The long period will no longer be oscillatory and short period pitch responses will decay to a pitch rate response proportional to the amount of elevator input; If slightly negative (Equivalent of moving CG behind the stick fixed neutral point); In the long period, elevator stick position will reverse, i.e., as speed increases a pull will be required on the elevator followed by a push, and as speed decreases, a push will be required followed by a pull The short period responses will result in a continuous divergence from the trim state. -
Vehicle Model for Tyre-Ground Contact Force Evaluation
Vehicle model for tyre-ground contact force evaluation Lejia Jiao Master Thesis in Vehicle Engineering Department of Aeronautical and Vehicle Engineering KTH Royal Institute of Technology TRITA-AVE 2013:40 ISSN 1651-7660 Postal address Visiting Address Telephone Telefax Internet KTH Teknikringen 8 +46 8 790 6000 +46 8 790 6500 www.kth.se Vehicle Dynamics Stockholm SE-100 44 Stockholm, Sweden Acknowledgment I owe gratitude to many people for supporting me during my thesis work. Especially, I would like to express my deepest appreciation to my supervisor, Associate professor Jenny Jerrelind, for her enthusiasm and infinite passion for this project. Without her patient guidance and persistent help, this thesis would not have been possible. I am particularly indebted to my parents for inspiring me to this work. I would like to thank Associate professor Lars Drugge, who introduced me to vehicle-road interaction and gave me enlightening instruction. In addition, I would like to give my sincere thanks to Nicole Kringos and Parisa Khavassefat, for helping me to understand the pavement and sharing model and data with me; to Ines Lopez Arteaga, for giving me feedbacks from tyre expert’s point of view. The great interdisciplinary cooperation and teamwork helped me to have a good understanding of the whole vehicle-tyre-pavement system, and get rational tyre and pavement parts included in my models. Last but not least, I would like to thank all my friends, for their understanding, encouragement and support. Stockholm June 26, 2013 Lejia Jiao i ii Abstract Economic development and growing integration process of world trade increases the demand for road transport. -
Introduction to Aircraft Stability and Control Course Notes for M&AE 5070
Introduction to Aircraft Stability and Control Course Notes for M&AE 5070 David A. Caughey Sibley School of Mechanical & Aerospace Engineering Cornell University Ithaca, New York 14853-7501 2011 2 Contents 1 Introduction to Flight Dynamics 1 1.1 Introduction....................................... 1 1.2 Nomenclature........................................ 3 1.2.1 Implications of Vehicle Symmetry . 4 1.2.2 AerodynamicControls .............................. 5 1.2.3 Force and Moment Coefficients . 5 1.2.4 Atmospheric Properties . 6 2 Aerodynamic Background 11 2.1 Introduction....................................... 11 2.2 Lifting surface geometry and nomenclature . 12 2.2.1 Geometric properties of trapezoidal wings . 13 2.3 Aerodynamic properties of airfoils . ..... 14 2.4 Aerodynamic properties of finite wings . 17 2.5 Fuselage contribution to pitch stiffness . 19 2.6 Wing-tail interference . 20 2.7 ControlSurfaces ..................................... 20 3 Static Longitudinal Stability and Control 25 3.1 ControlFixedStability.............................. ..... 25 v vi CONTENTS 3.2 Static Longitudinal Control . 28 3.2.1 Longitudinal Maneuvers – the Pull-up . 29 3.3 Control Surface Hinge Moments . 33 3.3.1 Control Surface Hinge Moments . 33 3.3.2 Control free Neutral Point . 35 3.3.3 TrimTabs...................................... 36 3.3.4 ControlForceforTrim. 37 3.3.5 Control-force for Maneuver . 39 3.4 Forward and Aft Limits of C.G. Position . ......... 41 4 Dynamical Equations for Flight Vehicles 45 4.1 BasicEquationsofMotion. ..... 45 4.1.1 ForceEquations .................................. 46 4.1.2 MomentEquations................................. 49 4.2 Linearized Equations of Motion . 50 4.3 Representation of Aerodynamic Forces and Moments . 52 4.3.1 Longitudinal Stability Derivatives . 54 4.3.2 Lateral/Directional Stability Derivatives . -
Car Suspension and Handling Fourth Edition
Car Suspension and Handling Fourth Edition List of Chapters: Preface to the Fourth Edition 3.8 Tire Uniformity 3.9 Aspect Ratios Preface to the First Edition 3.10 Tire Selection and Air Chamber Geometry Notation 3.11 References Chapter 1 Introduction Chapter 4 Steering 1.1 Scope and Layout of the Book 4.1 Dynamic Function of the Steering 1.2 The Function of the Suspension System System 4.2 Steering Angles: Effects of Tire Slip 1.3 Suspension Geometry Angles and Steering and Suspension 1.4 Kinematics and Compliance (K&C) Kinematics 1.5 Vehicle Dynamics 4.3 Relative Positions of Front- and Rear- 1.6 References Wheel Tracks 4.4 Understeer and Oversteer Chapter 2 Disturbances and Sensitivity 4.5 Directional Stability 2.1 Road Irregularities 4.6 Torque in the Steering System 2.2 Influence of Wheel Size 4.7 Steering Torque Effects Due to 2.3 Subjective Assessment of Ride Steering Geometry 2.4 Human Sensitivity to Vibration 4.8 The Steering Column 2.5 Measurement Standards for Vibration 4.9 Steering Gear 2.6 Influence of Noise on Assessment of 4.10 Constant Velocity (CV) Driveshaft Ride Comfort Joints 2.7 Influence of Phase of Differential 4.11 Torque Steer Effects Vibration on Assessment of Ride 4.12 Front-Wheel Steering Oscillations— Comfort Shimmy 2.8 References 4.13 Power Assistance 4.14 Electric Power Steering Chapter 3 The Wheel and Tire 4.15 Rear-Wheel Steering Systems 3.1 Introduction 4.16 References 3.2 The Wheel Rim 3.3 Tire Size Designation Chapter 5 Suspension Systems and 3.4 Tire Construction Types Their Effects 3.5 Tire Properties -
Static Stability and Control
CHAPTER 2 Static Stability and Control "lsn't it astonishing that all these secrets have been preserved for so many years just so that we could discover them!" Orville Wright, June 7, 1903 2.1 HISTORICAL PERSPECTIVE By the start of the 20th century, the aeronautical community had solved many of the technical problems necessary for achieving powered flight of a heavier-than-air aircraft. One problem still beyond the grasp of these early investigators was a lack of understanding of the relationship between stability and control as well as the influence of the pilot on the pilot-machine system. Most of the ideas regarding stability and control came from experiments with uncontrolled hand-launched gliders. Through such experiments, it was quickly discovered that for a successful flight the glider had to be inherently stable. Earlier aviation pioneers such as Albert Zahm in the United States, Alphonse Penaud in France, and Frederick Lanchester in England contributed to the notion of stability. Zahm, however, was the first to correctly outline the requirements for static stability in a paper he presented in 1893. In his paper, he analyzed the conditions necessary for obtaining a stable equilibrium for an airplane descending at a constant speed. Figure 2.1 shows a sketch of a glider from Zahm's paper. Zahm concluded that the center of gravity had to be in front of the aerodynamic force and the vehicle would require what he referred to as "longitudinal dihedral" to have a stable equilibrium point. In the terminology of today, he showed that, if the center of gravity was ahead of the wing aerodynamic center, then one would need a reflexed airfoil to be stable at a positive angle of attack. -
Approach for the Development of Suspensions with Integrated
Approach for the Development of Suspensions with Integrated Electric Motors Von der Fakultät Konstruktions-, Produktions- und Fahrzeugtechnik der Universität Stuttgart zur Erlangung der Würde eines Doktors der Ingenieurwissenschaften (Dr.-Ing.) genehmigte Abhandlung Vorgelegt von Meng Wang aus Hebei, China Hauptberichter: Prof. Dr. -Ing. Horst E. Friedrich Mitberichter: Prof. Dr. -Ing. Eckhard Kirchner Tag der mündlichen Prüfung: 06. May 2020 Institut für Verbrennungsmotoren und Kraftfahrwesen, Universität Stuttgart Angefertigt am Institut für Fahrzeugkonzepte, Deutsches Zentrum für Luft- und Raumfahrt (DLR) e.V. Stuttgart 2020 D93 (Dissertation Universität Stuttgart) Acknowledgments The author would like to thank his supervisors Prof. Dr. -Ing. Friedrich and Prof. Dr. - Ing. Kirchner for their consistent support and patience to his Ph.D study. The author is sincerely thankful to his advisor Dr. Elmar Beeh for his encouragement and guidance with his professional knowledge. Without their support, this thesis would not be completed. I am grateful to have these colleagues, who provided me honest communication and exchange of learning experience: Dr. Zhou Ping, Dr. Andreas Höfer, Dr. Diego Schierle, Dr. Jens König, Dr. Gerhard Kopp and so on. I wish to thank the support of colleagues in laboratory of DLR FK, who helped me to complete the test and acquired the useful data in this work: Michael Kriescher, Philipp Straßburger, Cedric Rieger and so on. I wish to thank these friendly colleagues: David Krüger, Lucia Areces Fernandez, Marco Münster, Erik Chowson, Thomas Grünheid and so on, who let me enjoy the work in DLR FK. You are already my best friends in Germany. I want to mention Moritz Fisher, Dr. -
Truck Handling Stability Simulation and Comparison of Taper-Leaf and Multi-Leaf Spring Suspensions with the Same Vertical Stiffness
applied sciences Article Truck Handling Stability Simulation and Comparison of Taper-Leaf and Multi-Leaf Spring Suspensions with the Same Vertical Stiffness Leilei Zhao 1, Yunshan Zhang 2, Yuewei Yu 1,*, Changcheng Zhou 1,*, Xiaohan Li 1 and Hongyan Li 3 1 School of Transportation and Vehicle Engineering, Shandong University of Technology, Zibo 255000, China; [email protected] (L.Z.); [email protected] (X.L.) 2 Shandong Automobile Spring Factory Zibo Co.,Ltd., Zibo 255000, China; [email protected] 3 State Key Laboratory of Automotive Simulation and Control, Jilin University, Changchun 130022, China; [email protected] * Correspondence: [email protected] (Y.Y.); [email protected] (C.Z.); Tel.: +86-135-7338-7800 (C.Z.) Received: 16 December 2019; Accepted: 31 January 2020; Published: 14 February 2020 Abstract: The lightweight design of trucks is of great importance to enhance the load capacity and reduce the production cost. As a result, the taper-leaf spring will gradually replace the multi-leaf spring to become the main elastic element of the suspension for trucks. To reveal the changes of the handling stability after the replacement, the simulations and comparison of the taper-leaf and the multi-leaf spring suspensions with the same vertical stiffness for trucks were conducted. Firstly, to ensure the same comfort of the truck before and after the replacement, an analytical method of replacing the multi-leaf spring with the taper-leaf spring was proposed. Secondly, the effectiveness of the method was verified by the stiffness tests based on a case study. Thirdly, the dynamic models of the taper-leaf spring and the multi-leaf spring with the same vertical stiffness are established and validated, respectively. -
Concept of Moving Centre of Gravity for Improved Directional Stability for Automobiles
IJIRST –International Journal for Innovative Research in Science & Technology| Volume 2 | Issue 11 | April 2016 ISSN (online): 2349-6010 Concept Of Moving Centre of Gravity for Improved Directional Stability for Automobiles - Simulation Joseph Sebastian Siyad S UG Student UG Student Department of Mechanical Engineering Department of Mechanical Engineering Saintgits College of Engineering Saintgits College of Engineering Subin Antony Jose Ton Devasia UG Student UG Student Department of Mechanical Engineering Department of Mechanical Engineering Saintgits College of Engineering Saintgits College of Engineering Prof. Sajan Thomas Professor Department of Mechanical Engineering Saintgits College of Engineering Abstract This paper is a study based on the implementation of a new concept in AUTOMOBILE which will help in improving the directional stability and handling characteristics of vehicle. The purpose of this study is to analyze the influence of position of CENTRE OF GRAVITY of a vehicle in its stability in accordance with YAW MOTION, ROLL MOTION, UNDER STEER and OVER STEER. The concept is to implement a mechanism which can bring SHIFTING OF C.G in automobile, as per the conditions. The influence of position of C.G is much bigger for the balancing of forces in dynamic stability of the vehicle. The concept of moving C.G will help to acquire this added stability to the vehicle even in the worst conditions.The directional stability of a vehicle is influenced by the steering angle and slip angle of the tire to an extent. It is possible to have a variation in these values by the shifting of CG. The designing of a convenient mechanism which helps in achieving the movement of the mass (either by pumping a high density fluid or my movement of a solid block by mechanical linkage) is to be done and have to be tested in a real time vehicle. -
L1262 Rev B 01-20 © 2016 – 2019 Hendrickson USA, L.L.C
THE EVOLUTION OF TRAILER SUSPENSION DAMPING: A GUIDE TO BEST PRACTICES The noticeable ride benefits of suspension damping devices also bring maintenance challenges for fleets. Educate yourself on the evolution of damping methods to better manage long-term costs. All vehicles, passenger or commercial, are designed with damping in mind when it comes to the suspension. The primary goal of a suspension system is to carry the load from the vehicle while providing compliance between the sprung mass (chassis, trailer body, etc.) and the unsprung mass (the suspension, tires, wheels, brakes, etc). Damping devices, such as shock absorbers, are designed to add comfort and control by resisting the motion of the suspension. Without damping forces, a vehicle would have a tendency to bounce at its natural, or resonant, frequency. But over the service life of the vehicle, most suspension damping devices result in a compromise of either ride quality or added component maintenance. In the commercial trailer industry, managing issues like driver comfort, cargo protection, vehicle safety and government compliance can be a complicated balancing act. Understanding the fundamentals of damping enables fleets to better manage long-term maintenance and operation costs while keeping ride quality and driver satisfaction high. What Is Damping and Why Do I Need It? Damping describes the process of absorbing energy of road inputs that are transmitted through the suspension system. Suspension damping reduces the number and intensity of these inputs to the vehicle thereby helping to prolong the life of the vehicle and its components. In turn, this helps reduce overall operating and maintenance costs. -
Design, Modelling & Analysis of Double Wishbone Suspension
International Journal on Mechanical Engineering and Robotics (IJMER) _______________________________________________________________________________________________ Design, Modelling & Analysis of Double Wishbone Suspension System 1Nikita Gawai, 2Deepak Yadav, 3Shweta Chavan, 4Apoorva Lele, 5Shreyash Dalvi Thakur College of Engineering & Technology, Kandivali (E), Mumbai-400101. Email: [email protected], [email protected], [email protected], [email protected], [email protected] Fig.1: Double wishbone Suspension system Abstract : The main objective of the project is to analyze the entire Double wishbone suspension system for Green F1 car, It is popular as front suspension mostly used in rear wheel as it allows the engineer to carefully control the motion of drive vehicles. Design of the geometry of double the wheel throughout suspension travel. A 3D CAD model of wishbone suspension system along with design of spring the Double wishbone is prepared by using SolidWorks plays a very important role in maintaining the stability of (CAD Software) for analyzing the system capable of handling Green F1 car while maintaining the ride quality. the vehicle. The topic is focused on designing the above mentioned suspension system considering the dynamics of the vehicle The upper arm is usually shorter to induce negative along with minimizing the unsprung mass. camber as the suspension jounces (rises), and often this arrangement is titled an "SLA” or Short Long Arms Index Terms—Roll center, Stiffness, Spring, Strut, Sprung suspension. When the vehicle is in a turn, body roll results ,Wishbone. in positive camber gain on the lightly loaded inside wheel, while the heavily loaded outer wheel gains negative I. INTRODUCTION camber. Suspension system is the term given to the system of The Four bar link mechanism formed by the unequal arm springs, shock absorbers and linkages that connect a lengths causes a change in the camber of the vehicle as it vehicle to its wheels. -
Stability and Control
Stability and Control AE460 Aircraft Design Greg Marien Lecturer Introduction Complete Aircraft wing, tail and propulsion configuration, Mass Properties, including MOIs Non-Dimensional Derivatives (Roskam) Dimensional Derivatives (Etkin) Calculate System Matrix [A] and eigenvalues and eigenvectors Use results to determine stability (Etkin) Reading: Nicolai - CH 21, 22 & 23 Roskam – VI, CH 8 & 10 Other references: MIL-STD-1797/MIL-F-8785 Flying Qualities of Piloted Aircraft Airplane Flight Dynamics Part I (Roskam) 2 What are the requirements? Evaluate your aircraft for meeting the stability requirements See SRD (Problem Statement) for values • Flight Condition given: – Airspeed: M = ? – Altitude: ? ft. – Standard atmosphere – Configuration: ? – Fuel: ?% • Longitudinal Stability: – CmCGα < 0 at trim condition – Short period damping ratio: ? – Phugoid damping ratio: ? • Directional Stability: – Dutch roll damping ratio: ? – Dutch roll undamped natural frequency: ? – Roll-mode time constant: ? – Spiral time to double amplitude: ? 3 Derivatives • For General Equations of Unsteady Motions, reference Etkin, Chapter 4 • Assumptions – Aircraft configuration finalized – All mass properties are known, including MOI – Non-Dimensional Derivatives completed for flight condition analyzed – Aircraft is a rigid body – Symmetric aircraft across BL0, therefore Ixy=Iyz = 0 – Axis of spinning rotors are fixed in the direction of the body axis and have constant angular speed – Assume a small disturbance • Results in the simplified Linear Equations of Motion…