Lift and drag improvements of airfoil through utilization of rough surface at trailing edge
It is well known that roughness effect is detrimental for the aerodynamics performance of a surface or airfoil in the sense that it produces higher drag and lower lift. However, literature study lead to the understanding (fact) that in low subsonic regime for free stream velocity Reynolds number be...
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| 第一著者: | |
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| フォーマット: | 学位論文 |
| 言語: | English |
| 出版事項: |
2014
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| オンライン･アクセス: | http://psasir.upm.edu.my/id/eprint/47985/1/FK%202014%2031R.pdf http://psasir.upm.edu.my/id/eprint/47985/ |
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