Increase in operating speeds and altitudes of pilotless aircraft has created need for basic aerodynamic data in hypersonic speed range; flow surveys show that single-expansion nozzle produces reasonably uniform flow with average free stream Mach number of 6.86. See also Engineering Index 1950 p 1302.


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    Title :

    Investigation of flow through single-stage two-dimensional nozzle in Langley 11-inch hypersonic tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    30 pages


    Remarks:

    Illus, Diagrs


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel

    MacLellan, Charles H. / Williams, Thomas W. / Beckwith, Ivan E. | TIBKAT | 1950



    Investigation of two-step nozzle in Langley 11-inch hypersonic tunnel

    McLellan, C.H. / Williams, T.W. / Bertram, M.H. | Engineering Index Backfile | 1950


    Investigation of a two-step nozzle in the Langley 11-inch hypersonic tunnel

    MacLellan, Charles H. / Williams, Thomas W. / Bertram, Mitchel H. | TIBKAT | 1950


    Investigation of a Two-step Nozzle in the Langley 11-inch Hypersonic Tunnel

    Mclellan, Charles Herbert / Williams, Thomas W / Bertram, Mitchel H | NTRS | 1950