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...
| मुख्य लेखक: | Mohamed Ahmed, Osman |
|---|---|
| स्वरूप: | थीसिस |
| भाषा: | अंग्रेज़ी अंग्रेज़ी |
| प्रकाशित: |
1997
|
| विषय: | |
| ऑनलाइन पहुंच: | http://psasir.upm.edu.my/id/eprint/10007/1/FK_1997_8_A.pdf |
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समान संसाधन
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प्रकाशित: (2014) -
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