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22911

Investigation of the Ride Response of a Multi-wheeled Combat Vehicle in Pitch-Bounce Plane

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Last updated: 04 Jan 2025

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Abstract

Recently there is a worldwide trend to transform the heavy troops into more agile and deployable forces. These forces are based on light armored multi-wheeled combat vehicles which are demanding several challenging requirements. Furthermore, the design of suspension system of these vehicles is complex and should provide several conflicting issues such as higher mobility and cornering stability whilst maintaining a sufficient ride comfort for the crew. This paper presents a comprehensive investigation of the ride response of a typical combat vehicle in pitch-bounce plan under the effect of random road excitation. A set of mathematical passive suspension models for the vehicle with different configurations including two-axle, three-axle and four-axle are derived. The numerical simulation is carried out through the MATLAB/SIMULINK environment which aids the future development of controllable suspension systems. The ride responses of the vehicle is obtained and analyzed considering the vibration isolation, suspension deflection, and road-holding. The results show an improvement in the responses of vehicle body vertical acceleration, pitch acceleration and
dynamic tire load using four-axle vehicle configuration over three-axle and two-axle ones.

DOI

10.21608/asat.2015.22911

Keywords

Vehicle ride dynamics, suspension system, half car model

Authors

First Name

M.

Last Name

Mohsen

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Affiliation

PhD Student, Automotive Engineering Dept., Military Technical College.

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First Name

H.

Last Name

Eltaher

MiddleName

M.

Affiliation

Lecturer, Automotive Engineering Dept., Military Technical College.

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First Name

A.

Last Name

Sharaf

MiddleName

M.

Affiliation

Associate Professor, Head of Automotive Engineering Dept., Military Technical College.

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First Name

S.

Last Name

El-demerdash

MiddleName

M.

Affiliation

Professor, Helwan University, Faculty of Engineering and Technology, Mataria, Cairo, Egypt.

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Volume

16

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015

Related Issue

4316

Issue Date

2015-05-01

Receive Date

2018-12-26

Publish Date

2015-05-01

Page Start

1

Page End

13

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_22911.html

Detail API

https://asat.journals.ekb.eg/service?article_code=22911

Order

22

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Investigation of the Ride Response of a Multi-wheeled Combat Vehicle in Pitch-Bounce Plane

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Article

Created At

22 Jan 2023