Aerodynamic computer code for calculating the pressure distribution on missile or its components e.g., body and wings and to interpolate by surface fit at locations as specified for structural analysis using the NASTRAN computer code. (Author)


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    Title :

    Aerodynamic Computer Code for Computing Pressure Loading on Complete Missile for Structural Analysis


    Contributors:
    K. K. Wang (author)

    Publication date :

    1978


    Size :

    208 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English