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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| Format: | Thèse |
| Langue: | anglais |
| Publié: |
2014
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| Accès en ligne: | http://eprints.usm.my/61101/ |
| Abstract | Abstract here |