Multi-Disciplinary computational aerospace sciences (MCAS): Preliminary studies on source panel method

Priya, P and Singh, Hema and Kulkarni, PS and Jha, RM (2008) Multi-Disciplinary computational aerospace sciences (MCAS): Preliminary studies on source panel method. Technical Report. National Aerospace Laboratories, Bangalore.

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Abstract

Panel methods are one of the popular numerical techniques for handling the fluid flows around complicated configurations like airplanes. Panel methods comprise of source panel and vortex panel methods. In the present report, source panel method is studied for the estimation of pressure distribution over a circular and elliptical cylinder by dividing the surface of the body into panels. Both the cases of inscribed and circumscribed panels are considered. The software code is developed for eight panels and the computed results are validated against those in open literature. The generalized version of the code was further developed increasing the number of panels to an optimum number.

Item Type: Proj.Doc/Technical Report (Technical Report)
Uncontrolled Keywords: Source panel;Pressure distribution;Panel methods;Circumscribed panels;Inscribed panel;Circular cylinder;Elliptical cylinder
Subjects: ENGINEERING > Electronics and Electrical Engineering
Division/Department: Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 27 Jul 2010 12:02
Last Modified: 27 Jul 2010 12:02
URI: http://nal-ir.nal.res.in/id/eprint/8784

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