Presence of tip reduces lift and performance compared with corresponding values for 2-dimensional wing; it appeared from work by K.STEWARTSON that addition of vane at wing tip might counteract this effect; effect due to presence of vane determined.


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    Titel :

    Effect of Delta vanes on supersonic wings


    Weitere Titelangaben:

    Aeronautical Quarterly


    Beteiligte:
    Gorgui, M.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1954


    Format / Umfang :

    29 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Delta wings for supersonic transport

    Jones, Jr., J.L. / Hunton, L.W. / Gregory, T.J. et al. | Engineering Index Backfile | 1963


    Supersonic aerodynamics of delta wings

    Wood, Richard M. | NTRS | 1988


    Supersonic Flutter of Cantilevered Delta Wings

    Surace, G. / Gili, P. / Institution of Engineers, Australia et al. | British Library Conference Proceedings | 1993


    Nonlinear Supersonic Potential Flow over Delta Wings

    B. Grossman / M. J. Siclarit | AIAA | 1981


    The nonlinear supersonic potential flow over delta wings

    GROSSMAN, B. / SICLARI, M. | AIAA | 1980