Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow

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Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow

In this paper attention is focussed on study of effect of Aspect ratio of the wing on roll moment derivatives at various angle of attack and Mach number for a Supersonic flow. It is been observed that there is a linear increment in rolling moment derivative with aspect ratio as well as with Angle...

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Bibliographic Details
Main Authors:	Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	IRA Publications 2016
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/50991/ http://irep.iium.edu.my/50991/3/Asha_Crasta_-IJAER.pdf

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