Research Catalog

  • Active load control during rolling maneuvers [microform] / Jessica A. Woods-Vedeler, Anthony S. Pototzky, and Sherwood T. Hoadley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1994]
    • 1994
  • Flutter analysis of composite box beams [microform] / Matthew Greenman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • An interactive software for conceptual wing flutter analysis and parametric study [microform] / Vivek Mukhopadhyay.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Aeroelastic calculations using CFD for a typical business jet model [microform] / Michael D. Gibbons.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1996]
    • 1996
  • Response of the alliance 1 proof-of-concept airplane under gust loads [microform] / A.S. Naser, A.S. Pototsky, and C.V. Spain ; [prepared ... under contract NAS1-96014].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
  • Hot-bench simulation of the active flexible wing wind-tunnel model [microform] / Carey S. Buttrill, Jacob A. Houck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64063
  • Digital-flutter-suppression-system investigations for the active flexible wing wind-tunnel model [microform] / Boyd Perry III ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69415
  • Static aeroelastic analysis of a three-dimensional generic wing [microform] / John A. Green, In Lee and Hirokazu Miura.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : For sale by the National Technical Information Service, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69417
  • Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model [microform] / Walter A. Silva and Robert M. Bennett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69438
  • Transonic calculations for a flexible supercritical wing and comparison with experiment [microform] / Robert M. Bennett, David A. Seidel, Maynard C. Sandford.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
  • 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
  • Research, technology, and engineering accomplishments, 2014 : advancing technology and science through flight.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Neil A. Armstrong Flight Research Center, 2014.
    • 2014
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55376
  • 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
  • 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
  • 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

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