Determination of pressure distribution on a finite wing by kuchemann and weber method

Gopalakrishnan, AR and Ramamoorthy, P (1977) Determination of pressure distribution on a finite wing by kuchemann and weber method. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    A FORTRAN IV program for determining the13; pressure distribution on a finite wing is developed13; and presented here for any user. This software13; is based on the work of Kuchemann and weber and13; valid only for the incompressible flow. Conparisons13; with experiments and a sophisticated method like Multhopp's lifting surface theory have been made This quick method can be utilised for wing design also when hooked with an optimization program.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Finite wing;Lifting surface theory
    Subjects: MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
    AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Deputy Head Poornima Narayana
    Date Deposited: 30 Aug 2006
    Last Modified: 24 May 2010 09:48
    URI: http://nal-ir.nal.res.in/id/eprint/2506

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