Investigation conducted in Langley rectangular high speed tunnel on five supersonic airfoils and, for comparison, on two subsonic airfoils; two-dimensional data obtained by pressure measurements and Schlieren photographs at angles of attack from 0° to 4° for Mach numbers between 0.30 and 0.90 for these 6% thick symmetrical airfoils.


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    Title :

    Flow and force characteristics of supersonic airfoils at high subsonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    15 pages


    Remarks:

    41 Supp Plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    The Flow and Force Characteristics of Supersonic Airfoils at High Subsonic Speeds

    Lindsey, W F / Daley, Bernard N / Humphreys, Milton D | NTRS | 1947


    Inviscid flow about airfoils at high supersonic speeds

    Eggers, A. J. / Syvertson, Clarence A. | TIBKAT | 1952


    Inviscid flow about airfoils at high supersonic speeds

    Eggers, Jr., A.J. / Syvertson, C.A. | Engineering Index Backfile | 1952


    Inviscid flow about airfoils at high supersonic speeds

    Eggers, A J , Jr / Syvertson, Clarence A | NTRS | 1952