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

Monis, Renita Sharon and Shabana, Ayesha and Crasta, Asha and Khan, Sher Afghan (2017) Computation of stiffness derivative for an unsteady delta wing with curved leading edges. International Journal of Recent Research Aspects .., 4 (4). pp. 69-72. ISSN 2349-7688

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Abstract

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 increases the stiffness derivative also increases. This is an improvement of previous theory as the effect of leeward surface are included in the present work.

Item Type:	Article (Journal)
Additional Information:	7395/61843
Uncontrolled Keywords:	Unsteady, Hypersonic, Delta wing, Curved leading edge
Subjects:	Q Science > QA Mathematics > QA297 Numerical Analysis
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User:	Prof. Dr. Sher Afghan Khan
Date Deposited:	05 Feb 2018 15:43
Last Modified:	05 Feb 2018 15:43
URI:	http://irep.iium.edu.my/id/eprint/61843

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