Investigations carried out by Guggenheim Aeronautics Laboratory at California Institute of Technology on effects of boundary layer transition phenomena and surface roughness on drag; results of this investigation show that apparatus developed for measuring wing section drags in flight is practical and is amenable to quick adaptation to full scale airplane. Before Inst Aeronautical Sciences.


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    Title :

    Boundary layer and wake survey measurements in flight and in wind tunnel


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1940


    Size :

    9 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :