Previous report gave calculations for pressure distribution over thin oblique airfoils at supersonic speed; present report extends calculations to subsonic speeds; it is found that flows again can be obtained by superposition of elementary conical flow fields; in case of sweepback wing pressure distributions remain qualitatively similar at subsonic and supersonic speeds. See also Engineering Index 1946 p 23.


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    Title :

    Subsonic flow over thin oblique airfoils at zero lift


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Jones, R.T. (author)


    Publication date :

    1947


    Size :

    13 pages


    Remarks:

    7 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :