Investigation of transonic aerodynamic performance characteristics of six nozzles using hot jet exhaust provided by hydrogen peroxide system; 12-tube and 12-lobe nozzles had lowest internal losses at static conditions and 8-lobe nozzle with centerbody, shroud, and secondary air had least propulsive losses.


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    Title :

    Transonic performance characteristics of several jet noise suppressors


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    48 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Transonic Performance Characteristics of Several Jet Noise Suppressors

    Schmeer, James W. / Salters, Leland B., Jr. / Cassetti, Marlowe D. | NTRS | 1960


    Transonic Performance Characteristics of Several Jet Noise Suppressors

    J. W. Schmeer / L. B. Salters / M. D. Cassetti | NTIS | 1960


    Transonic performance characteristics of several jet noise suppressors

    Schmeer, James W. / Salters, Leland B. / Cassetti, Marlowe D. | TIBKAT | 1960



    Transonic drag of several jet-noise suppressors

    North, W.J. | Engineering Index Backfile | 1958