Computation of stiffness derivative for an unsteady delta wing with curved leading edges

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Computation of stiffness derivative for an unsteady delta wing with curved leading edges

An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number increases. It is also seen that as amplitude of half sine wave i...

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Bibliographic Details
Main Authors:	Monis, Renita Sharon, Shabana, Ayesha, 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/61843/ http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf

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