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Landing gear loads analysis
Anthony Jr., Seth Russell
Anthony Jr., Seth Russell
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t1964_Anthony,Jr.pdf
Adobe PDF, 6.78 MB
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1964-04
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Thesis
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Electronic dissertations
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Abstract
A method is developed to predict the non-linear effects of oleo strut landing gears with the aid of a digital computer. The method is applied to two illustrative examples. The first example is a proposed articulated oleo strut landing gear. The results obtained, using computer studies, are used to determine the feasibility or manufacturing such a landing gear. The second example is presented to illustrate that this technique can predict, quite accurately, test results. This latter example is used to support the validity of the analysis.
Table of Contents
Notation -- Summary -- Introduction -- Analysis -- Articulated landing gear example -- Comparison with experimental data -- Conclusions -- References -- Figures -- Computer program
Description
Thesis (M.S.)-- University of Wichita, College of Engineering, Dept. of Aeronautical Engineering
Publisher
Wichita State University
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Wichita State University