Research carried out at Ames Research Center with respect to configuration for which serious problems have been foreseen; some results of performance studies are considered relating to wing loading effects, effects of thrust-to-weight ratio, and engine air inlets; investigation at low subsonic speeds is in progress to study effectiveness of various high lift devices applied to delta wing configuration; full span plain flap applied to wing leading edge was effective in increasing maximum lift-drag ratio: other factors studied.


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    Titel :

    Delta-wing configurations for supersonic transport


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Jones, Jr., J.L. (Autor:in) / Hunton, L.W. (Autor:in) / Gregory, T.J. (Autor:in) / Nelms, Jr., W.P. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    DELTA-WING CONFIGURATIONS FOR THE SUPERSONIC TRANSPORT

    Gregory, T. J. / Hunton, L. W. / Jones, J. L., Jr. et al. | NTRS | 1963


    A Critical Study of Delta-Wing Configurations for the Supersonic Transport Application

    J. L. Jones, Jr. / L. W. Hunton / T. J. Gregory et al. | NTRS | 1963


    A CRITICAL STUDY OF DELTA-WING CONFIGURATIONS FOR THE SUPERSONIC TRANSPORT APPLICATION

    Gregory, T. J. / Hunton, L. W. / Jones, J. L., Jr. et al. | NTRS | 1963