Methods of thin airfoil theory have been extended to oblique or swept back airfoils of finite aspect ratio moving at supersonic speeds; cases considered are symmetrical airfoils at zero lift having plan forms bounded by straight lines.


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    Title :

    Thin oblique airfoils at supersonic speed


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Jones, R.T. (author)


    Publication date :

    1946


    Size :

    21 pages


    Remarks:

    12 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Thin oblique airfoils at supersonic speed

    Jones, Robert T. | TIBKAT | 1946


    Thin oblique airfoils at supersonic speed

    Jone, Robert T | NTRS | 1946


    Thin Oblique Airfoils at Supersonic Speed

    Jones, Robert T | NTRS | 1946