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: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Wings;Supersonic flow
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    Division/Department: Fluid Mechanics
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 06 Aug 2012 11:25
    Last Modified: 06 Aug 2012 11:25

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