Computational analysis of double rotating cylinders for conceptual design of an estol, fixed wing UAV
Many efforts in Unmanned Aerial Vehicle (UAV) aerodynamic design technology led to a broad of additional applications. Magnus effect is the effect of moving airstream to the spinning ball or cylinder. Previous studies revealed the feasibility of Magnus effect on rotating cylinder producing lift whic...
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| フォーマット: | 学位論文 |
| 言語: | 英語 |
| 出版事項: |
2017
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| 主題: | |
| オンライン･アクセス: | http://psasir.upm.edu.my/id/eprint/76076/1/FK%202018%20156.pdf |