Wind-tunnel tests were conducted on a 0.175-scale model of the OMAC Laser 300 canard configuration in the NASA Langley 12-Foot Low-Speed Wind Tunnel to determine its low-speed high angel-of-attack aerodynamic characteristics. The Laser 300 is a general aviation turboprop pusher aircraft utilizing a canard configuration. The design incorporates a low forward wing and a high main wing with a leading-edge droop installed on the outboard panel and tip fins mounted on the wing tips. The model was tested over a range of -6 to 50-deg angle-of-attack and 20 to -20 deg sideslip. Static force and moment data were measured, and the longitudinal and lateral-directional characteristics were determined.


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    Titel :

    Wind-tunnel investigation of the OMAC canard configuration


    Beteiligte:
    Ingram, W. C. (Autor:in) / Yip, L. P. (Autor:in) / Cook, E. L. (Autor:in)

    Erscheinungsdatum :

    01.09.1986


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Wind-tunnel investigation of the OMAC canard configuration

    INGRAM, W. / YIP, L. / COOK, E. | AIAA | 1986


    Wind-Tunnel Investigation of an Advanced General Aviation Canard Configuration

    J. R. Chambers / L. P. Yip / T. M. Moul | NTIS | 1984


    Wind-Tunnel Investigation of an Advanced General Aviation Canard Configuration

    Chambers, J. R. / Yip, L. P. / Moul, T. M. | NTRS | 1984



    WIND TUNNEL TEST RESULTS FOR A CANARD ROTOR/WING AIRCRAFT CONFIGURATION

    Thompson, T. L. / Smith, R. L. / Helwani, M. et al. | British Library Conference Proceedings | 2001