Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges

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Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges

The present study focuses attention on the effect of Aspect ratio of the wing on roll damping moment derivative at various angles of attack and Mach number has been studied. It is found that rolling moment derivative increases with aspect ratio as well as with the angle of attack as the rolling mome...

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Bibliographic Details
Main Authors:	Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	IMRF Journals 2015
Subjects:	QA Mathematics TL500 Aeronautics TL780 Rockets
Online Access:	http://irep.iium.edu.my/46635/ http://irep.iium.edu.my/46635/1/46635.pdf

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