An Experimental Study Of Oscillating Subboundary Layer Vortex Generators Application On A Wing'S Flap
Flow control to suppress the boundary layer separation over the wmg can dramatically improve the performance of most aircraft in the take-off and lancling flight regime. Previous aerodynamic experiments and computations have indicated that unsteady excitation produced by the oscillating sub bound...
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| 格式: | Thesis |
| 語言: | 英语 |
| 出版: |
2014
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| 在線閱讀: | http://eprints.usm.my/61101/ |
| Abstract | Abstract here |