Pressure distribution and damping in steady pitch at supersonic mach numbers of flat swept-back wings having all edges subsonic.


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    Title :

    Pressure distribution and damping in steady pitch at supersonic mach numbers of flat swept-back wings having all edges subsonic


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    62 pages


    Remarks:

    Diagrs


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :