Aerodynamic data for the DFVLR R4 airfoil are presented in both graphic and tabular form. The R4 was tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel (TCT) at Mach number from 0.60 to 0.78 at angles of attack from -2.0 to 8.0 degrees. The airfoil was tested at Reynolds numbers of 4, 6, 10, 15, 30, and 40 million based on the 152.32 mm chord.


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    Title :

    Data from tests of a R4 airfoil in the Langley 0.3-meter transonic cryogenic tunnel


    Contributors:

    Publication date :

    1984-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :