An inlet technology development program for future supersonic cruise aircraft is in progress. Areas being emphasized are inlet aerodynamic and control system design requirements for efficient and reliable operation. Off-design conditions, such as angle of incidence, starting, and noise abatement are major considerations. Flow analysis procedures are being developed to predict the internal inviscid and viscous flows in axisymmtric supersonic inlets for these operating conditions. Also under development are control systems that will have significant interfaces with the engine control system, the flight control system, and the airframe avionics system. The analytical methods are being supported and validated with representative experiments.


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    Titel :

    Inlet design technology development - Supersonic cruise research


    Beteiligte:
    Syberg, J. (Autor:in) / Paynter, G. C. (Autor:in) / Carlin, C. M. (Autor:in)

    Kongress:

    Joint Propulsion Conference ; 1981 ; Colorado Springs, CO, US


    Erscheinungsdatum :

    01.07.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Inlet design technology development - Supersonic cruise research

    SYBERG, J. / PAYNTER, G. / CARLIN, C. | AIAA | 1981


    Supersonic Cruise Technology

    F. E. McLean | NTIS | 1985


    Supersonic Cruise Technology

    Mclean, F. Edward | NTRS | 1985


    Supersonic cruise Technology

    MacLean, F. E. / USA, National Aeronautics and Space Administration | TIBKAT | 1985


    Inlet design studies for a Mach 2.2 advanced supersonic cruise vehicle

    SHIMABUKURO, K. / WELGE, H. / LEE, A. | AIAA | 1979