The NASA High Speed Research (HSR) Program is intended to establish a technology base enabling industry development of an economically viable and environmentally acceptable second generation high speed civil transport (HSCT). The objective of the Configuration Aerodynamics task of the program is the development of aerodynamic drag reduction, stability and control, and propulsion airframe integration technologies required to support the HSCT development process. Aerodynamic design tools are being developed, evaluated, and validated through ground based experimental testing. In addition, methods for ground to flight scaling are being developed and refined.


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    Titel :

    High Reynolds Number Predictions for the Baseline Arrow Wing at Mach 2.48


    Beteiligte:
    Rivers, Melissa (Autor:in) / Wahls, Richard (Autor:in)


    Erscheinungsdatum :

    01.12.1999


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    New high Reynolds number Mach 8 capability

    HEDLUND, ERIC R. / HIGGINS, CRAIG W. / ROZANSKI, CHARLES S. et al. | AIAA | 1992



    Some effects of Reynolds number on a cambered wing at high subsonic Mach numbers

    Gamble, H. E. / Aeronautical Research Council | TIBKAT | 1952