Extension to the Panel Code NALSOP0509 to Include Design of Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment

Desai, SS and Narayana, CL and Rangarajan, R (1985) Extension to the Panel Code NALSOP0509 to Include Design of Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    The code NALSOP0509, available in the SOFFTS Library of NAL has been extended to include a design of wing-body combinations to, minimize induced drag for specified lift and pitching moments at sub- or super--sonic flow conditions, Method of Lagrangean multiple is used to obtain the optimum camber and twist distributions for the wing in the presence of a body. SOFFTS Library of NAL has now been updated with this version of the code.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Wing design;Combat configurations;Drag optimization;Panel method
    Subjects: AERONAUTICS > Aerodynamics
    MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 27 Sep 2012 14:40
    Last Modified: 27 Sep 2012 14:40
    URI: http://nal-ir.nal.res.in/id/eprint/11030

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