Development of tunnel in which test Mach numbers from 0.6 to slightly over 1.0 are achieved by rotating test model in annular passage between two concentric cylinders. Supersedes declassified NACA RM L8A23, Rm L50E18, and RM L9G19.


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    Title :

    Langley annular transonic tunnel


    Additional title:

    NACA -- Report


    Contributors:
    Habel, L.W. (author) / Henderson, J. (author) / Miller, M.F. (author)


    Publication date :

    1952


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    The Langley Annular Transonic Tunnel

    Habel, Louis W / Henderson, James H / Miller, Mason F | NTRS | 1952


    The Langley annular transonic tunnel

    Habel, Louis W. / Henderson, James H. / Miller, Mason F. | TIBKAT | 1952




    Rotorcraft aeroelastic testing in the Langley Transonic Dynamics Tunnel

    Yeager, W.T. jun. / Mirick, P.H. / M-Nabil H. Hamouda et al. | Tema Archive | 1993