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...
Saved in:
主要作者: | |
---|---|
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!
|