Investigation of temperature recovery factors carried out in continuous type wind tunnel at Naval Supersonic Laboratory of MIT. Bibliography.


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    Title :

    Experimental determination of flat plate recovery factors for Mach numbers between 1.90 and 3.14


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1954


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :