The NASA-Langley Research Center is currently investigating the high angle-of-attack characteristics of a forward-swept wing fighter technology demonstrator in a cooperative program with the Defense Advanced Research Projects Agency. The program includes static and dynamic wind-tunnel force tests, free-flight model tests, spin-tunnel tests, and piloted simulation. Particular emphasis is placed on identifying the contributions of the forward-swept wing to the configuration aerodynamics at high angles of attack. Results are presented to illustrate the wing contributions in terms of aerodynamic stability, flow visualization, and observation of free-flight characteristics.


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    Titel :

    High angle-of-attack characteristics of a forward-swept wing fighter configuration


    Beteiligte:
    Grafton, S. B. (Autor:in) / Gilber, W. P. (Autor:in) / Croom, M. A. (Autor:in) / Murri, D. G. (Autor:in)

    Kongress:

    Atmospheric Flight Mechanics Conference ; 1982 ; San Diego, CA


    Erscheinungsdatum :

    1982-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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