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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| Main Author: | |
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| Format: | Thesis |
| Language: | English |
| Published: |
2014
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| Subjects: | |
| Online Access: | http://eprints.usm.my/61101/1/24%20Pages%20from%2000001785045.pdf |
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