The development of four wings which were designed to have specific aerodynamic requirements is described. The wings designed were: a high lift wing, a low lift or cruise wing, both of which were smooth, and two flapped wings which were approximations of the smooth wings.


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    Titel :

    High Lift Surface Design Procedures. Experimental Verification. Volume II. Theoretical Design and Analysis


    Beteiligte:
    J. R. Stevens (Autor:in) / J. W. McDonald (Autor:in) / J. W. Headley (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    STOL High-Lift Design Study. Volume II. Bibliography

    F. May / C. A. Widdison | NTIS | 1971


    Advanced high lift design through analytical/experimental techniques

    BRADEN, J. / BARNETT, L. / HOLMES, A. et al. | AIAA | 1975


    CD volume design and verification

    Li, Y. / Hughes, J. | AIAA | 1993


    High lift airfoil design method, high lift airfoil and aircraft

    YUAN MENG / QI SHIBING / QIN YOUHUA et al. | Europäisches Patentamt | 2023

    Freier Zugriff