Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges

Dutt, HNV (1986) Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    This project document is a User's manual for computer13; program for calculating the longitudinal aerodynamic13; characteristics of wing-body-tail combinations in subsonic flows and at angles of attack for which symmetrical pairs13; of vortices are shed from the body nose and leading edge13; and side edges of the lifting surfaces.13; This document contains a short description of the method,13; instructions for preparation of input and program listing.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Vortex lattice method;Symmetrical vortex shedding;Suction analogy
    Subjects: MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
    AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: Deputy Head Poornima Narayana
    Date Deposited: 28 Aug 2006
    Last Modified: 24 May 2010 09:48
    URI: http://nal-ir.nal.res.in/id/eprint/2381

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