The flight trajectory analysis on the existing aircraft
This thesis presents the flight trajectory analysis for a given aircraft configuration starting with aircraft set at trim condition and after that following by descent for landing. It has been known that the aircraft behaviors during their flight governed by the flight equation of motions. This f...
| 第一著者: | |
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| フォーマット: | 学位論文 |
| 言語: | 英語 英語 英語 |
| 出版事項: |
2012
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| 主題: | |
| オンライン･アクセス: | http://eprints.uthm.edu.my/2143/ |
| Abstract | Abstract here |