Computer program computes zero lift wave drag of an entire aircraft including any combination of the wing, body, pods, fins, and carnard. The program computes the external volume of the wing and the axial area distribution of the wing equivalent body.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Program computes zero lift wave drag of entire aircraft


    Contributors:

    Publication date :

    1967-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Program Computes Thermodynamic Functions

    Mcbride, Bonnie J. / Gordon, Sanford | NTRS | 1994




    Program Computes Dendrite-Settling Velocities

    De Groh, Henry, III / Weidman, Patrick / Zakhem, Riad et al. | NTRS | 1994