A series of wind-tunnel tests were conducted in a V/STOL tunnel to determine the low-speed longitudinal aerodynamic characteristics of a powered close-coupled wing/canard fighter configuration. The data was obtained for a high angle-of-attack maneuvering configuration and a takeoff and landing configuration. The data presented in tabulated form are intended for reference purposes.


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    Titel :

    Effect of Twist and Camber on the Low-Speed Aerodynamic Characteristics of a Powered Close-Coupled Wing-Canard Configuration


    Beteiligte:
    J. W. Paulson (Autor:in) / J. L. Thomas (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    159 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch