Study, made to evaluate various methods of minimizing overall pressure ratio required to establish and maintain full expansion of nozzle flow, investigating cylindrical diffusers, diffusers with contraction and diffusers including right-angle turn; results obtained are summarized.


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    Title :

    Experimental evaluation of rocket exhaust diffusers for altitude simulation


    Additional title:

    NASA -- Tech Note


    Contributors:
    Sivo, J.N. (author) / Meyer, C.L. (author) / Peters, D.J. (author)


    Publication date :

    1960


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Experimental evaluation of rocket exhaust diffusers for altitude simulation

    Sivo, Joseph N. / Meyer, Carl L. / Peters, Daniel J. | TIBKAT | 1960



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