Computation of stability derivatives of an oscillating cone for specific heat ratio = 1.66

In this paper the expressions for stiffness and Damping derivatives are obtained in a closed form for perfect gas where the flow is quasi-steady and axi-axisymmetric, and the nose semi angle of the cone is such that the Mach number behind the shock . Results are presented for an oscillating cone...

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Bibliographic Details

Main Authors:	Shabana, Aysha, Monis, Renita Sharon, Crasta, Asha, Khan, Sher Afghan
Format:	Proceeding Paper
Language:	en
Published:	Institute of Physics Publishing 2018
Subjects:	TJ Mechanical engineering and machinery TJ255 Heat engines
Online Access:	http://irep.iium.edu.my/66482/1/66482_Computation%20of%20Stability%20Derivatives%20of%20an%20oscillating_article.pdf http://irep.iium.edu.my/66482/ http://iopscience.iop.org/article/10.1088/1757-899X/370/1/012059/meta
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