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: | , |
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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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