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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.
Elmas Atabay, Ibrahim Ozkol. 2012. "Stability analysis of a landing gear mechanism with torsional degree of freedom". Global Journal of Research in Engineering GJRE-D Volume 12 (GJRE Volume 12 Issue D1).
Crossref Journal DOI 10.17406/gjre
Print ISSN 0975-5861
e-ISSN 2249-4596
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Total Score: 107
Country: Turkey
Subject: Global Journal of Research in Engineering
Authors: Dr. Elmas Atabay, Ibrahim Ozkol (PhD/Dr. count: 1)
View Count (all-time): 466
Total Views (Real + Logic): 1951
Total Downloads (simulated): 96
Publish Date: 2012 01, Sun
Monthly Totals (Real + Logic):
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