Research Catalog

  • Mission information and test systems summary of accomplishments, 2011 / Sean E. McMorrow and Roberta B. Sherrard.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo41404
  • An indirect system identification technique for stable estimation of continuous-time parameters of the vestibulo-ocular reflex (VOR) / Sunil L. Kukreja, Ragnar Wallin, Richard D. Boyle.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, NASA Dryden Flight Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo41413
  • Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50963
  • Virtual deformation control of the X-56A model with simulated fiber optic sensors / Peter M. Suh and Alexander W. Chin, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50964
  • Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove / Trong T. Bui.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50966
  • An overview of NASA's Subsonic Research Aircraft Testbed (SCRAT) / Ethan Baumann, Joe Hernandez, and John C. Ruhf.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, October 2013.
    • 2013-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54678
  • Modal filtering for control of flexible aircraft / Peter M. Suh, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54680
  • Survey of applications of active control technology for gust alleviation and new challenges for lighter-weight aircraft / Christopher D. Regan and Christine V. Jutte.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2012.
    • 2012-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32723
  • Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane / Frank W. Burcham, Jr. [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, October 1997.
    • 1997-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67454
  • A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing / Ming H. Tang and Robert G. Sheldon.

    • Text
    • Edwards California : NASA Dryden Flight Research Center, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71159
  • Estimation of modal parameters using a wavelet-based approach / Rick Lind, Marty Brenner, and.Sydney M. Haley.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Fligh Research Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78991
  • Design and evaluation of a new boundary layer rake for flight testing / Trong T. Bui and David L. Oates, Jose c. Gonsalez.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo85536
  • A real-time method for estimating viscous forebody drag coefficients / Stephen A. Whitmore [and three others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo85540
  • Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results / Arild Bertelrud [and ten others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo85548
  • Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius / Thomas J. Horn, Amanie N. Abdelmessih.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, August 2000.
    • 2000-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS31291
  • Optimal pitch thrust-vector angle and benefits for all flight regimes / Glenn B. Gilyard, Alexander Bolonkin.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, March 2000.
    • 2000-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85803
  • Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness / Stephen A. Whitmore.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo86340
  • Design of low complexity model reference adaptive controllers / Curt Hanson [and three others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33464
  • Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test / Christine V. Jutte [and five others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo34104
  • Flight test results on the stability and control of the F-15 Quiet Spike aircraft / Cheng M. Moua [and three others].

    • Text
    • Edwards, CA : National Aeronautics and, Space Administration, Dryden Flight Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32721
  • Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37308
  • First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37309
  • In-flight boundary-layer transition on a large flat plate at supersonic speeds / D.W. Banks [and four others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37503
  • Orion Pad Abort 1 Crew Module mass properties test approach and results / Claudia Herrera and Adam Harding.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37504
  • Frequency shift during mass properties testing using compound pendulum method / David Wolfe and Chris Regan.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37507
  • Sensor-only system identification for structural health monitoring of advanced aircraft / Sunril L. Kukreja, Dennis S. Bernstrein.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, NASA Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37509
  • Thermostructural analysis of the SOFIA fine field and wide field imagers subjected to convective thermal shock / Christopher B. Kostyk.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37512
  • Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / Percy J. Bobbitt [and four others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37677

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