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  Linear Static and Fatigue Analysis of Nose Landing Gear for Trainer Aircraft

  By Ashwin C. Gowda, Novid Basha S

  Abstract: The main objective of this paper is to present prototype of aircraft landing gear using CATIA V5 software to study the behavior of landing gear as per actual working condition and to perform structural analysis to study the landing gear behavior for cyclic loading (fatigue loading). Determining the loading modes in the nose landing gear is subjected to static load and cyclic loads which should be taken into account in …

  Published in Journal of Mechatronics and Automation · Vol. 1, Issue 2, 2014 · pp. 1–10 Read article →