Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow

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Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow

n the present paper a theory for 2D slender bodies at high angle of attack in hypersonic flow has been developed to determine the aerodynamic derivatives in pitch for different Mach numbers. The present theory has been applied to a sharp thick wedge with attached shock case. Using the theory, a rela...

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Bibliographic Details
Main Authors:	Shanbhag, Pavithra, Lavanya, S, Khan, Sher Afghan, Crasta, Asha
Format:	Article
Language:	English
Published:	Indian Society for Education and Environment & Informatics Publishing Limited 2016
Subjects:	QB Astronomy
Online Access:	http://irep.iium.edu.my/53877/ http://irep.iium.edu.my/53877/1/SAKHAN.pdf

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