Operating characteristics of 5° conical flow expander investigated in Lewis 2×2-ft Mach 3.88 tunnel to determine whether or not its use would establish full supersonic flow; results indicate that method should be practical.


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    Title :

    Three-dimensional flow expander as device to increase Mach number in supersonic wind tunnel


    Additional title:

    NASA -- Memo


    Contributors:
    Salmi, R.J. (author)


    Publication date :

    1958


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Mach Number 6 Capability for AEDC Supersonic Wind Tunnel (16S), Requirements and Concepts

    Steinle, F. W. / Hawkins, W. R. / Mills, M. L. et al. | British Library Conference Proceedings | 2004





    FEASIBILITY OF OPERATING THE AEDC SUPERSONIC WIND TUNNEL (16S) UP TO MACH NUMBER 6

    Mills, M. L. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004