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