Estimation of stability derivatives of a delta wing in hypersonic flow

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Estimation of stability derivatives of a delta wing in hypersonic flow

In the present study supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for attached shock case. A strip theory is used in which strips at different span wise locations are independent. This combines with similitude to give a piston theory. The pres...

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Bibliographic Details
Main Authors:	Crasta, Asha, Baig, Maugal Ahmed Ali, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	RS Publication 2012
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL787 Astronautics
Online Access:	http://irep.iium.edu.my/49933/ http://irep.iium.edu.my/49933/1/52-paper7.pdf

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