Method of analysis, based upon superposition of series of conical and quasiconical fields of pressure derived from linear theory.


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    Title :

    Pressure distribution and damping in steady roll at supersonic mach numbers of flat swept-back wings with subsonic edges


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    57 pages


    Remarks:

    Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :