Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges

Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges

In the Present paper effect of angle of incidence on Stiffness derivative of a delta wing with Curved leading edges for attached shock case in Supersonic Flow has been studied. A Strip theory is used in which strips at different span wise location are independent of each other. This combines with si...

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Bibliographic Details
Main Authors: Crasta, Asha, Khan, Sher Afghan
Format: Article
Language:English
Published: International Organozation of Scientific Research (IOSR) Journals 2014
Subjects:
TL787 Astronautics
Online Access:http://irep.iium.edu.my/49935/
http://irep.iium.edu.my/49935/1/49935.pdf

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