Comparison of Linear and Nonlinear Dampers for Landing Gears
01 Oct 1978-Journal of Aircraft (American Institute of Aeronautics and Astronautics (AIAA))-Vol. 15, Iss: 10, pp 696-698
About: This article is published in Journal of Aircraft.The article was published on 1978-10-01. It has received None citation(s) till now. The article focuses on the topic(s): Damper & Landing gear.
01 Jan 1953
TL;DR: In this article, a theoretical study of the behavior of the conventional oleo-pneumatic landing gear during the process of landing impact is presented in a general form and treats the motions of the landing gear prior to and subsequent to the beginning of shock-strut deflection.
Abstract: This report presents a theoretical study of the behavior of the conventional type of oleo-pneumatic landing gear during the process of landing impact. The basic analysis is presented in a general form and treats the motions of the landing gear prior to and subsequent to the beginning of shock-strut deflection. The applicability of the analysis to actual landing gears has been investigated for the particular case of a vertical landing gear in the absence of drag loads by comparing calculated results with experimental drop-test data for impacts with and without tire bottoming. The calculated behavior of the landing gear was found to be in good agreement with the drop-test data.
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