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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主要作者: | Mohamed Ahmed, Osman |
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格式: | Thesis |
语言: | English English |
出版: |
1997
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在线阅读: | http://psasir.upm.edu.my/id/eprint/10007/1/FK_1997_8_A.pdf http://psasir.upm.edu.my/id/eprint/10007/ |
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