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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| Pengarang-pengarang Utama: | , , |
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| Format: | Artikel |
| Bahasa: | English |
| Diterbitkan: |
RS Publication
2012
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| Subjek-subjek: | |
| Capaian Atas Talian: | http://irep.iium.edu.my/49933/ http://irep.iium.edu.my/49933/ http://irep.iium.edu.my/49933/1/52-paper7.pdf |
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