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Analysis and Optimization of Incompressible Inviscid Flow around Split Flap Airfoils

Generally airfoils are designed for cruise flight conditions; but during take-off and landing, when the airplane flies at low speeds and small angles of attacks, the lift provided by single airfoils is not sufficient, and an extra lift is required for safe landing and take-off. In this condition...

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書目詳細資料
主要作者:	Mohamed Ahmed, Osman
格式:	Thesis
語言:	English English
出版:	1997
在線閱讀:	http://psasir.upm.edu.my/id/eprint/10007/1/FK_1997_8_A.pdf http://psasir.upm.edu.my/id/eprint/10007/
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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