Oscillating supersonic delta wings with curved leading edges

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Oscillating supersonic delta wings with curved leading edges

In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. This combines with the similitude to give a piston theo...

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Bibliographic Details
Main Authors:	Khan, Sher Afghan, Crasta , Asha
Format:	Article
Language:	English
Published:	The Jangjeon Mathematical Society (JMS) 2010
Subjects:	QA75 Electronic computers. Computer science
Online Access:	http://irep.iium.edu.my/49812/ http://irep.iium.edu.my/49812/1/asha-crasta.pdf

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