Two procedures for calculating lift distribution along span given, in which better account is taken of distribution of circulation over area than in Prandtl lifting line theory. English translation from ZWB Forschungsbericht n 1533 Feb 27 1942.


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    Title :

    Lift distribution of swept-back wings


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1947


    Size :

    38 pages


    Remarks:

    10 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Theoretical lift of flat swept-back wings at supersonic speeds

    Cohen, D. | Engineering Index Backfile | 1948


    On chordwise lift distribution at centre of swept wings

    Kuechemann, D. / Weber, J. | Engineering Index Backfile | 1950



    Pressure-distribution measurements on unyawed swept-back wings

    Jacobs, W. | Engineering Index Backfile | 1947


    Methods of reducing transonic drag of swept-back wings at zero lift

    Kuchemann, D. | Engineering Index Backfile | 1957