Estimation of stability derivative of an oscillating cone in hypersonic flow
Formulae for the Stiffness and Damping derivatives are obtained in a closed form in the present context with the assumptions that the gas is non-viscous and perfect, the motion is quasi-steady and quasi-axisymmetric, and the nose semi angle of the cone is such that the Mach number M2 behind the sh...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Institute of Institutional Industrial Research
2017
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/61839/ http://irep.iium.edu.my/61839/ http://irep.iium.edu.my/61839/1/Paper2-IJRRA-04-04-14.pdf |