Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
In the present study hypersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with curved leading edges for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. This combines with the similitude...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
International Association of Engineering and Management Education (IAEME)
2012
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49929/ http://irep.iium.edu.my/49929/ http://irep.iium.edu.my/49929/1/ESTIMATION_OF_STABILITY_DERIVATIVES_OF_AN_OSCILLATING_HYPERSONIC_DELTA_WINGS_WITH_CURVED-paper10.pdf |