The effects of geometric design parameters on the internal performance of nonaxisymmetric single expansion-ramp nozzles were investigated at nozzle pressure ratios up to approximately 10. Forward-flight (cruise), vectored-thrust, and reversed-thrust nozzle operating modes were investigated.


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    Title :

    Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing


    Contributors:
    Re, R. J. (author) / Berrier, B. L. (author)

    Publication date :

    1982-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



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