Estimation of stability derivative of an oscillating cone in hypersonic flow

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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...

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Bibliographic Details
Main Authors:	Shabana, Ayesha, Monis, Renita Sharon, Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	Institute of Institutional Industrial Research 2017
Subjects:	QA297 Numerical Analysis
Online Access:	http://irep.iium.edu.my/61839/ http://irep.iium.edu.my/61839/1/Paper2-IJRRA-04-04-14.pdf

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