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  • A Preliminary investigation of the use of throttles for emergency flight control [microform] / F. W. Burcham, Jr. ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
    • 1991

  • Flight-determined benefits of integrated flight-propulsion control systems [microform] / James F. Stewart, Frank W. Burcham, Jr., and Donald H. Gatlin.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992

  • Flight-determined engine exhaust characteristics of an F404 engine in an F-18 airplane [microform] / Kimberly A. Ennix, Frank W. Burcham. Jr., and Lannie D. Webb.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplane [microform] / Frank W. Burcham, Jr. ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Development and flight evaluation of an emergency digital flight control system using only engine thrust on an F-15 airplane [microform] / Frank W. Burcham, Jr. ... [et. al].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Using engine thrust for emergency flight control [microform] : MD-11 and B-747 results / Frank W. Burcham ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Simulator evaluation of simplified propulsion-only emergency flight control systems on transport aircraft [microform] / Frank W. Burcham ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane [microform] / Frank W. Burcham, Jr. ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Propulsion flight research at NASA Dryden from 1967 to 1997 [microform] / Frank W. Burcham, Jr. ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Minimum time and fuel flight profiles for an F-15 airplane with a highly integrated digital electronic control system [microform] / Edwward A. Haering, Jr. and Frank W. Burcham, Jr.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Preliminary flight test results of the F100 EMD engine in an F-15 airplane [microform] / Lawrence P. Myers and Frank W. Burcham, Jr.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1984]
    • 1984

  • Comparison of results obtained from flight tests and simulated tests of a digital electronic engine control system on an F-15 airplane [microform] / Lawrence P. Myers and Frank W. Burcham, Jr.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1983]
    • 1983

  • Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests / Jon K. Holzman, Lannie D. Webb, and Frank W. Burcham, Jr.

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66654

  • Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / Frank J. Kurtenbach and Frank W. Burcham, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
    • 1981-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71438

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