Research Catalog

  • Large-deformation displacement transfer functions for shape predictions of highly flexible slender aerospace structures / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55847
  • Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2013.
    • 2013-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49705
  • Coherent lidar turbulence measurement for gust load alleviation / David Soreide [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66616
  • F-15B/flight test fixture II : a test bed for flight research / David M. Richwine.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65685
  • Design and integration of an actuated nose strake control system / Bradley C. Flick [and five others].

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66653
  • 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
  • F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack / Andrew J. Yuhas [and three others].

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66655
  • Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack / Kevin R. Walsh [and three others].

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, April 1997.
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66657
  • Nonstationary dynamics data analysis with wavelet-SVD filtering / Marty Brenner, Dale Groutage.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2001.
    • 2001-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22782
  • Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 / Mark C. Davis [and five others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, May 2000.
    • 2000-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85555
  • Developing uncertainty models for robust flutter analysis using ground vibration test data / Starr Potter and Rick Lind.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2001.
    • 2001-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22840
  • Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack / Brent R. Cobleigh, Mark A. Croom.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, May 2001.
    • 2001-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS30134
  • Reconfigurable control design for the full X-33 flight envelope / M. Christopher Cotting and John J. Burken.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, August 2001.
    • 2001-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS26814

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