Studies of transition over flat plate at Mach Number 1.76 carried out using hot wire anemometer as one of principal tools; nature and measurements of free stream disturbance at supersonic speeds, analyzed; results interpreted in light of present overall information on transition at supersonic speeds; conclusions as to further experiments.


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    Title :

    On transition experiments at moderate supersonic speeds


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1957


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :