'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds

Ramamoorthy, P and Premageetha, BK (1991) 'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    An existing computer software package for the determination of lift, drag and pitching moment of the finite wing is ported onto PS 386/387 system and,validated against known examples. This software is presently designated as AEROWING and is used to obtain the loads on the wing of an RPV (Remotely piloted Vehicle).quot; 13; The results prove that the software can provide a tool for the wing analysis amp; design.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aerofoil;Pressure distribution;Finite wing
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 11 Oct 2006
    Last Modified: 24 May 2010 09:51
    URI: http://nal-ir.nal.res.in/id/eprint/2942

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