Effect of angle of incidence on stability derivatives of a wing

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Effect of angle of incidence on stability derivatives of a wing

In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. A Strip theory is used in which strips at different span wise location are independent. This combines with similitude to give a piston theory....

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Bibliographic Details
Main Authors:	Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	http://www.ijraset.com/fileserve.php?FID=491 2014
Subjects:	TL787 Astronautics
Online Access:	http://irep.iium.edu.my/49938/ http://irep.iium.edu.my/49938/1/49938.pdf

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