Laminar boundary layer and position of transition point were investigated on heated flat plate; it was found that Reynolds number of transition decreases as temperature of plate is increased.


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    Title :

    Investigations of effects of surface temperature and single roughness elements on boundary-layer transition


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Liepmann, H.W. (author) / Fila, G.H. (author)


    Publication date :

    1947


    Size :

    17 pages


    Remarks:

    14 Supp Plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :