Pressure distribution and pressure drag were determined on body which had jet issuing from nose at several free stream Mach numbers; as result of retrorocket operation large decrease in pressure drag occurred; at same time, retrorocket caused very unstable flow about model.


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    Title :

    Investigation of retrorocket exhausting from nose of blunt body into supersonic free stream


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English