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F. W. Burcham   Mechanical engineering, energy technology   Physics   Clear all
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    Landing Approach Airframe Noise Measurements and Analysis

    P. L. Lasagna / K. G. Mackall / F. W. Burcham et al. | NTIS | 1980
    Keywords: Aircraft landing , Aircraft noise , Aircraft configurations , Landing gear

    Preliminary Investigation of the Use of Throttles for Emergency Flight Control

    F. W. Burcham / C. G. Fullerton / G. B. Gilyard et al. | NTIS | 1991
    Keywords: Aircraft , Aircraft control , Aircraft landing , Boeing 720 aircraft , F-15 aircraft

    Controlling Crippled Aircraft-with Throttles

    F. W. Burcham / C. G. Fullerton | NTIS | 1991
    Keywords: Aircraft , Aircraft control , Aircraft landing , Boeing 720 aircraft , F-15 aircraft , Jet aircraft , Transport aircraft

    Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control

    F. W. Burcham / T. Maine / T. Wolf | NTIS | 1992
    Keywords: Aircraft , Aircraft landing , F-15 aircraft

    Flight Test of a Propulsion Controlled Aircraft System on the NASA F-15 Airplane

    F. W. Burcham / T. A. Maine | NTIS | 1995
    Keywords: Aircraft control , Aircraft performance , F-15 aircraft , Aircraft landing , Aircraft maneuvers

    Design Challenges Encountered in the F-15 PCA Flight Test Program

    T. A. Maine / F. W. Burcham / P. Schaefer et al. | NTIS | 1995
    Keywords: Aircraft control , Aircraft landing , F-15 aircraft , Research aircraft

    Flight Test of a Propulsion-Based Emergency Control System on the MD-11 Airplane with Emphasis on the Lateral Axis

    J. J. Burken / F. W. Burcham / T. A. Maine et al. | NTIS | 1996
    Keywords: Aircraft , Aircraft control , Md 11 aircraft , Aircraft landing

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