Stability analysis of a landing gear mechanism with torsional degree of freedom

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Elmas Atabay
Elmas Atabay
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Dr. Elmas Atabay
Dr. Elmas Atabay
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Ibrahim Ozkol
Ibrahim Ozkol
α Istanbul Technical University Istanbul Technical University

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Stability analysis of a landing gear mechanism  with torsional degree of freedom

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Abstract

In this study, stability of a landing gear mechanism with torsional degree of freedom is analyzed. Derivation of the equations of motion of the model with torsional degree of freedom and the von Schlippe tire model are presented. Nonlinear model is linearized and Routh-Hurwitz criterion is applied. Stability analysis is conducted in the e-v plane for different values of the torsional spring rate c and in the k-v plane for different values of the relaxation length σ and vertical force Fz . Percentages of the stable regions are computed. Effects of the variation of the caster length e, half contact length a and their ratio on stable regions are analyzed. Results and conclusions about the variation of stability are presented and constructive recommendations are given.

References

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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Elmas Atabay. 2012. \u201cStability analysis of a landing gear mechanism with torsional degree of freedom\u201d. Global Journal of Research in Engineering - D: Aerospace Science GJRE-D Volume 12 (GJRE Volume 12 Issue D1): .

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Version of record

v1.2

Issue date

February 25, 2012

Language
en
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In this study, stability of a landing gear mechanism with torsional degree of freedom is analyzed. Derivation of the equations of motion of the model with torsional degree of freedom and the von Schlippe tire model are presented. Nonlinear model is linearized and Routh-Hurwitz criterion is applied. Stability analysis is conducted in the e-v plane for different values of the torsional spring rate c and in the k-v plane for different values of the relaxation length σ and vertical force Fz . Percentages of the stable regions are computed. Effects of the variation of the caster length e, half contact length a and their ratio on stable regions are analyzed. Results and conclusions about the variation of stability are presented and constructive recommendations are given.

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Stability analysis of a landing gear mechanism with torsional degree of freedom

Dr. Elmas Atabay
Dr. Elmas Atabay
Ibrahim Ozkol
Ibrahim Ozkol

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