Computer program calculates effects on lift and drag of blowing two jets over swept tapered wing at low subsonic speeds. Algorithm used in based on vortex lattice representation of wing lifting surface on line source-sink distribution to represent effects of exhaust jets.


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    Title :

    Swept-tapered-wing aerodynamics


    Contributors:

    Published in:

    Publication date :

    1976-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


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