Arc chamber results on effects of rocket nozzle throat diameter and nozzle axial station on flow characteristics for Mach numbers from 12 to 26


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    Title :

    Calibration experience in the Langley hotshot tunnel for Mach numbers from 12 to 26


    Contributors:

    Publication date :

    1966-02-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English