Oscillating supersonic delta wing with straight leading edges

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Oscillating supersonic delta wing with straight leading edges

A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. Ghosh’s strip theory is been used in which strips at different span wise locations are independent of each other. This combines with the s...

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Bibliographic Details
Main Authors:	Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	IJCER 2012
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/49942/ http://irep.iium.edu.my/49942/1/JO2512261233-print-paper8.pdf

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