Pressure distributions on nozzle block of two-dimensional, oblique-exit-plane nozzle with turbulent flow were predicted and experimentally measured; thrusts, thrust vectors, and torques were calculated from pressure distributions; performance characteristics were strongly dependent upon plenum and ambient pressures and upon exit plane orientations; because of exit plane area changes, axial and lateral thrusts were found to exceed symmetric nozzle thrust values for certain conditions; results were predicted well by theory of characteristics and Gadd's formula for flow separation; at high altitudes, torque that can be obtained may be useful for maneuvering.


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    Title :

    Thrust vectoring produced by supersonic nozzle with oblique exit plane


    Additional title:

    J Spacecraft Rockets


    Contributors:
    Dunn, B.M. (author) / Emery, A.F. (author)

    Published in:

    Publication date :

    1966


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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