Oscillating supersonic delta wings with curved leading edges
In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing 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 to give a piston theo...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
The Jangjeon Mathematical Society (JMS)
2010
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49812/ http://irep.iium.edu.my/49812/ http://irep.iium.edu.my/49812/1/asha-crasta.pdf |