Based on experience from flight tests of swept aircraft, possible methods are discussed for determining, from wind tunnel test, maximum obtainable lift coefficient for landing; this is found difficult since dynamic effects in actual flight are not present in wind tunnel; based on available wind tunnel data approximate calculation of obtainable lift for landing is carried through for swept wing aircraft with various wing planforms; prevention of tip stall.


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    Title :

    Maximum lift for landing of swept wing aeroplanes


    Additional title:

    Svenska Aeroplan Aktibolaget -- Tech Note


    Contributors:
    Palme, H.O. (author)


    Publication date :

    1953


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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