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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    Titel :

    Maximum lift for landing of swept wing aeroplanes


    Weitere Titelangaben:

    Svenska Aeroplan Aktibolaget -- Tech Note


    Beteiligte:
    Palme, H.O. (Autor:in)


    Erscheinungsdatum :

    1953


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Tandem-wing aeroplanes

    Crowe, J.H. | Engineering Index Backfile | 1935


    Tandem-Wing Aeroplanes

    Crowe, J.H. | Emerald Group Publishing | 1935


    The landing of aeroplanes

    Glauert, Hermann | SLUB | 1920


    The landing of aeroplanes

    Alston, R. P. ;Bryant, L. W. ;Jones, I. M. W. | TIBKAT | 1934