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...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1998
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| Online Access: | http://ndltd.ncl.edu.tw/handle/40256121329338987406 |