Integration of propulsion and flight control systems and their optimization offers significant performance improvements. Research programs were conducted which have developed new propulsion and flight control integration concepts, implemented designs on high-performance airplanes, demonstrated these designs in flight, and measured the performance improvements. These programs, first on the YF-12 airplane, and later on the F-15, demonstrated increased thrust, reduced fuel consumption, increased engine life, and improved airplane performance; with improvements in the 5 to 10 percent range achieved with integration and with no changes to hardware. The design, software and hardware developments, and testing requirements were shown to be practical.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Propulsion system-flight control integration and optimization: Flight evaluation and technology transition


    Beteiligte:

    Kongress:

    AIAA 26th Joint Propulsion Conference ; 1990 ; Orlando, FL, United States


    Erscheinungsdatum :

    1990-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Propulsion system-flight control integration-flight evaluation and technology transition

    Burcham, Frank W., Jr. / Gilyard, Glenn B. / Myers, Lawrence P. | NTRS | 1990


    Propulsion system-flight control integration-flight evaluation and technology transition

    BURCHAM, JR., FRANK / GILYARD, GLENN / MYERS, LAWRENCE | AIAA | 1990


    Flight/propulsion control system integration

    EMERSON, L. / DAVIES, W. | AIAA | 1983


    Rotorcraft Flight-Propulsion Control Integration

    J. R. Mihaloew / M. G. Ballin / D. G. C. Ruttledge | NTIS | 1988