Typical airframe/propulsion interactions such as Mach/altitude excursions and inlet unstarts are reviewed. The improvements in airplane performance and flight control that can be achieved by improving the interfaces between propulsion and flight control are estimated. A research program to determine the feasibility of integrating propulsion and flight control is described. This program includes analytical studies and YF-12 flight tests.


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    Titel :

    Potential benefits of propulsion and flight control integration for supersonic cruise vehicles


    Beteiligte:
    Berry, D. T. (Autor:in) / Schweikhard, W. G. (Autor:in)


    Erscheinungsdatum :

    1976-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch