Operating characteristics are established for range of pressures and weight flows which allow ejector to be used as pump on discharge end of hypersonic blowdown wind tunnel; limited data on starting characteristics of open and closed test sections and effects of bluff body size on flow are presented.


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    Title :

    Experimental operating performance of single-stage annular air ejector


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :