Aerodynamic analysis of groove based vortex trap configuration on the retreating helicopter blade

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Aerodynamic analysis of groove based vortex trap configuration on the retreating helicopter blade

The issue of high angle of attacks at the retreating blade receives attention from countless researchers because it is an important factor in the stability of the helicopter. The retreating blade stall will effect the stability of the helicopter due to the high angle of attacks. Prouty‟s helicopter...

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Bibliographic Details
Main Author:	Yaakub, Mohd Fauzi
Format:	Thesis
Language:	English English English
Published:	2019
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://eprints.uthm.edu.my/30/ http://eprints.uthm.edu.my/30/1/24p%20MOHD%20FAUZI%20BIN%20YAAKUB.pdf http://eprints.uthm.edu.my/30/2/MOHD%20FAUZI%20BIN%20YAAKUB%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/30/3/MOHD%20FAUZI%20BIN%20YAAKUB%20WATERMARK.pdf

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