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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    Titel :

    Data from Tests of a R4 Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel


    Beteiligte:
    R. V. Jenkins (Autor:in) / W. G. Johnson (Autor:in) / A. S. Hill (Autor:in) / R. Mueller (Autor:in) / G. Redeker (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    356 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch