Oscillating supersonic delta wing with straight leading edges
A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. Ghosh’s strip theory is been used in which strips at different span wise locations are independent of each other. This combines with the s...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
IJCER
2012
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49942/ http://irep.iium.edu.my/49942/ http://irep.iium.edu.my/49942/1/JO2512261233-print-paper8.pdf |