Results on NACA 4412 section indicate that pressure distribution is practicaly unaffected by changes in Reynolds Number except where separation is involved. (10¢)


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    Title :

    Variations with Reynolds number of pressure distribution over airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1938


    Size :

    20 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Airfoil section characteristics as affected by variations of Reynolds Number

    Jacobs, E.N. / Sherman, A. | Engineering Index Backfile


    Airfoil section characteristics as affected by variations of Reynolds Number

    Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937


    Airfoil section characteristics as affected by variations of Reynolds Number

    Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937