Aerodynamic analysis of NAL Light Aircraft Wing using a vortex lattice program

Srivastava, A and Sharma, N and Srinivasa, C (1991) Aerodynamic analysis of NAL Light Aircraft Wing using a vortex lattice program. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    A litting analysis of NAL-LA wing has been made using a vortex lattice program and the aexA3;quot;odynamic characteristics are computed by modelling the wing as a system of horse shoe vortices. The spanwise loading shows close agreement with elliptic loading and the section lift coefficient is nearly constant across the span except at the wing tip. The aerodynamic characteristics exhibit satisfactory convergence with increasing panel density.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Vortex;Lattice
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    AERONAUTICS > Aerodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mr. N A
    Date Deposited: 28 Jun 2006
    Last Modified: 24 May 2010 09:44
    URI: http://nal-ir.nal.res.in/id/eprint/1842

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