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