Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge

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Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge

Accurate estimation of the aerodynamic stability derivatives of airplanes is essential to evaluate the performance of the aircraft, whether civilian or military. Theoretical prediction methods for the dynamic stability derivatives at high angles of attack have not advanced, and in the present paper...

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Bibliographic Details
Main Authors:	Renita, sharon Monis, Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Transstellar Journal Publications and Research Consultancy Private Limited (TJPRC) 2019
Subjects:	QA297 Numerical Analysis
Online Access:	http://irep.iium.edu.my/75483/ http://irep.iium.edu.my/75483/1/2-67-1571463142-IJMPERDOCT201922.pdf http://irep.iium.edu.my/75483/7/75483_Estimation%20of%20damping%20derivatives_scopus.pdf

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