An Experimental Study Of Oscillating Subboundary Layer Vortex Generators Application On A Wing'S Flap

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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:	TK1-9971 Electrical engineering. Electronics. Nuclear engineering
Online Access:	http://eprints.usm.my/61101/ http://eprints.usm.my/61101/1/24%20Pages%20from%2000001785045.pdf

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