It is concluded that effect of sweepback is to increase area of stable laminar flow and to decrease lift coefficient at which flow separation occurs.


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    Title :

    Effects of sweepback on boundary layer and separation


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Jones, R.T. (author)


    Publication date :

    1947


    Size :

    6 pages


    Remarks:

    2 Supp Sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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