The needs and reasons for performing full-scale subsonic research have been studied. Full-scale wind-tunnel requirements are described; recommended size, airspeed, acoustic capabilities, and flow quality are developed; and data-acquisition systems, productivity, automation, and some cost elements are discussed. It is proposed that the optimum full-scale, subsonic wind tunnel be large enough to accommodate aerodynamic and acoustic investigations on most advanced aircraft, which exhibit complex engine/lifting-surface flow-field interactions, including advanced rotorcraft.


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    Titel :

    Optimum full-scale subsonic wind tunnel


    Beteiligte:
    Mort, K. W. (Autor:in) / Soderman, P. T. (Autor:in) / Meyn, Larry A. (Autor:in)

    Erscheinungsdatum :

    01.03.1986


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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