Dynamic Response of an Aircraft Flap Reducer

碩士 === 國立中山大學 === 機械工程研究所 === 86 === An aircraft flap gear reducer with an auxiliary power supply system is studied in this thesis. The dynamic model for the aircraftflap gear reducer system is developed by employing Lagrange's equation.Dynamic responses of the system is solved by us...

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Bibliographic Details
Main Authors: Tsai Ming Hwn, 蔡銘湖
Other Authors: Kuang Jao-Hwa
Format: Others
Language:zh-TW
Published: 1998
Online Access:http://ndltd.ncl.edu.tw/handle/40256121329338987406

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