Application of Program Laws to LCA Planforms

Dutta, Vimala (1988) Application of Program Laws to LCA Planforms. Project Report. National Aerospace Laboratories, Bangalore.

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This report presents the results of the computational work carried out for the lift analysis of LCA wings in supersonic flows using a computer software called LAWS [1]. The lifting pressure distribution and the associated force coefficients have been obtained for three planforms specified by the LCA group.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Wings;Supersonic flow
Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 06 Aug 2012 05:55
Last Modified: 06 Aug 2012 05:55

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