This test on the Lockheed designed 25 foot diameter X-Wing rotor had four purposes: (1) to expand the operating envelope to tip speeds of 700 ft/sec. and CT/o of .20; (2) to investigate track and balance sensitivities; (3) to evaluate the control system response characteristics at the higher disc loading; (4) to correlate CCHAP and CRUISE 4 analytical predictions with test data; and (5) to evaluate downwash on the close proximity fuselage.


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    Titel :

    X-Wing 25 Foot Diameter Lockheed Model Whirl Test Report


    Beteiligte:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    223 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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