Stability derivatives of a delta wing with straight leading edge in the Newtonian limit

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Stability derivatives of a delta wing with straight leading edge in the Newtonian limit

This paper presents an analytical method to predict the aerodynamic stability derivatives of oscillating delta wings with straight leading edge. It uses the Ghosh similitude and the strip theory to obtain the expressions for stability derivatives in pitch and roll in the Newtonian limit. The prese...

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Bibliographic Details
Main Authors:	Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	IJERA 2013
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL780 Rockets
Online Access:	http://irep.iium.edu.my/49939/ http://irep.iium.edu.my/49939/1/G43023238-paper9.pdf

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