The XFV-12A, a unique V/STOL technology prototype aircraft being developed for the Navy, is described. The innovative design features a thrust augmented wing and a canard ejector. Structural, functional, and control test performances are discussed. Static tether test results are also discussed. Assessment of test results are given along with projections for future modification areas.


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    Titel :

    The XFV-12A Thrust-Augmented Wing (TAW) prototype aircraft


    Beteiligte:
    Murphy, R. (Autor:in) / Lewis, E. L. (Autor:in)


    Erscheinungsdatum :

    01.09.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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