Study is part of program to study aspects of jet interference; variables involved were nozzle configuration and position beneath wing, and pressure ratio; design procedure for rockets used is given; incremental normal force due to jet interference on wing varied from one to 2 times rocket thrust and generally decreased as pressure ratio increased.


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    Title :

    Pressure loads produced on flat-plate wing by rocket jets exhausting in spanwise direction below wing and perpendicular to free-stream flow of mach number 2.0


    Additional title:

    NASA -- Tech Note


    Contributors:
    Falanga, R.A. (author) / Janos, J.J. (author)


    Publication date :

    1961


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English