The SR-71 test bed aircraft is shown to be a unique platform to flight-test large experiments to supersonic Mach numbers. The test bed hardware mounted on the SR-71 upper fuselage is described. This test bed hardware is composed of a fairing structure called the "canoe" and a large "reflection plane" flat plate for mounting experiments. Total experiment weights, including the canoe and reflection plane, as heavy as 14,500 lb can be mounted on the aircraft and flight-tested to speeds as fast as Mach 3.2 and altitudes as high as 80,000 ft. A brief description of the SR-71 aircraft is given, including details of the structural modifications to the fuselage, modifications to the J58 engines to provide increased thrust, and the addition of a research instrumentation system. Information is presented based on flight data that describes the SR-71 test bed aerodynamics, stability and control, structural and thermal loads, the canoe internal environment, and reflection plane flow quality. Guidelines for designing SR-71 test bed experiments are also provided.


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    Titel :

    The SR-71 Test Bed Aircraft: A Facility for High-Speed Flight Research


    Beteiligte:
    Corda, Stephen (Autor:in) / Moes, Timothy R. (Autor:in) / Mizukami, Masashi (Autor:in) / Hass, Neal E. (Autor:in) / Jones, Daniel (Autor:in) / Monaghan, Richard C. (Autor:in) / Ray, Ronald J. (Autor:in) / Jarvis, Michele L. (Autor:in) / Palumbo, Nathan (Autor:in)

    Erscheinungsdatum :

    2000-06-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    S. Corda / T. R. Moes / M. Mizukami et al. | NTIS | 2000


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