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...

書誌詳細
第一著者:	Mohamed Ahmed, Osman
フォーマット:	学位論文
言語:	英語英語
出版事項:	1997
主題:	Flaps (Airplanes) - Aerofoils - Analysis - Case studies
オンライン･アクセス:	http://psasir.upm.edu.my/id/eprint/10007/1/FK_1997_8_A.pdf

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