A 10%-scale Common Research Model-high lift version (CRM-HL) was developed to support extensive experimental investigations in the areas of active flow control, control surface optimization for landing and take-off, acoustic technology development, and computational fluid dynamics code validation to name a few. The CRM-HL was designed to have modular components that will enable the model to be tested in the following three forms: (1) conventional high-lift (CHL) configuration, (2) Active Flow Control (AFC) enabled simple hinged flap high-lift (SHL) configuration, and (3) CHL configuration with noise reduction treatments for the slats and/or the flaps. This paper describes the design, analysis, and fabrication of the CRM-HL for testing in the NASA Langley Research Center (LaRC) 14 by 22-Foot Subsonic Tunnel (14x22) and other wind tunnels as deemed appropriate by the research community such as the Qinetiq 5 Meter tunnel.


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    Titel :

    Development of the 10% NASA CRM High-Lift Common Research Model (CRM-HL)


    Beteiligte:
    Jared S. Fell (Autor:in) / Sandy R. Webb (Autor:in) / Christopher T. Laws (Autor:in) / Miranda L. Snyder (Autor:in) / Ray D. Rhew (Autor:in)

    Kongress:

    AIAA SciTech Forum ; 2021 ; Online, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Development of the NASA 10% High-Lift Common Research Model (CRM-HL)

    Fell, Jared / Webb, Sandy R. / Laws, Christopher T. et al. | AIAA | 2021


    DEVELOPMENT OF THE NASA 10% HIGH-LIFT COMMON RESEARCH MODEL (CRM-HL)

    Fell, Jared / Webb, Sandy R. / Laws, Christopher T. et al. | TIBKAT | 2021


    Large Eddy Simulation of the NASA High-Lift Common Research Model

    Goc, Konrad / Bose, Sanjeeb T. / Moin, Parviz | TIBKAT | 2022


    Large Eddy Simulation of the NASA High-Lift Common Research Model

    Goc, Konrad / Bose, Sanjeeb T. / Moin, Parviz | AIAA | 2022