Estimation of stability derivatives of a delta wing in hypersonic flow
In the present study supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for attached shock case. A strip theory is used in which strips at different span wise locations are independent. This combines with similitude to give a piston theory. The pres...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
RS Publication
2012
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49933/1/52-paper7.pdf http://irep.iium.edu.my/49933/ http://www.rspublication.com/ijeted/ijeted_index.htm |
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