Supersonic flow analysis and evaluation of damping derivative
The emphasis of this paper is to examine the variation of damping derivative with incidence angle and Mach number with varying pivot position. The damping derivative decreases with Mach number and increases with the incidence angle. It is also seen that for a given Mach number the damping derivative...
| Main Authors: | Monis, Renita Sharon, Shabana, Ayesha, Crasta, Asha, Khan, Sher Afghan |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
International Organization of Scientific Research ( IOSR )
2016
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/54297/ http://irep.iium.edu.my/54297/1/Renita.pdf |
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