Analysis of Stress and Displacement of Landing Gear for an Aircraft Through the Finite Element Method

Authors

  • Siva Sankar Kanchi  M. Tech Student, Department of Mechanical Engineering, GATES Engineering College, Gooty, Andhra Pradesh, India
  • C. Subhahan Basha  Assistant Professor, Department of Mechanical Engineering, GATES Engineering College, Gooty, Andhra Pradesh, India
  • Dr. P. Naresh   Assistant Professor and Head, Department of Mechanical Engineering, GATES Engineering College, Gooty, Andhra Pradesh, India

Keywords:

Aircraft Landing Gear System, TAIL DRAGGER, Ar 234 jet

Abstract

An aircraft landing gear system must absorb the kinematic energy produced by a landing impact and excitations caused by the aircraft travelling over an uneven runway surface. This is necessary requirement of successfully designed landing system. The oleo pneumatic shock is the most common type of shock absorber landing gear system used in aircraft. It dissipates the kinetic energy produced by impact arising when an airplane lands at high speed but also offer a comfortable rice to passenger when the airplane taxies at low speed. The objective of this project to determine the stress behavior and the displacement of a nose gear of an aircraft during landing using structural finite element analysis using with the help of analytical calculation. The external forces were determine analytical and the interactions between components were carefully modeled using contact analysis.

References

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International Journal of Scientific Research in Science and Technology

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Published

2022-04-30

Issue

Volume 9, Issue 2, March-April-2022

Section

Research Articles

License

Copyright (c) IJSRST

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This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

[1]
Siva Sankar Kanchi, C. Subhahan Basha, Dr. P. Naresh "Analysis of Stress and Displacement of Landing Gear for an Aircraft Through the Finite Element Method" International Journal of Scientific Research in Science and Technology(IJSRST), Online ISSN : 2395-602X, Print ISSN : 2395-6011,Volume 9, Issue 2, pp.237-251, March-April-2022.