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  • Transient hot-film sensor response in a shock tube [microform] / A.S. Roberts, Jr., K.R. Ortgies, and E. Gartenberg.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Substructive coupling in the frequency domain [microform] : a report to NASA Marshall Space Flight Center / by Randall C. Bachmeyer, Roy R. Craig, Jr.

    • Text
    • Austin Tex. : Center for Aeronautical Research, Bureau of Engineering Research, University of Texas at Austin ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • A transient FETI methodology for large-scale parallel implicit computations in structural mechanics [microform] / by C. Farhat, L. Crivelli, and F.X. Roux.

    • Text
    • Boulder, Colo. : Center for Space Structures and Controls, College of Engineering, University of Colorado ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Dynamic simulation of a wave rotor topped turboshaft engine [microform] / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Rotordynamics on the PC [microform] : further capabilities of ARDS / David P. Fleming.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Modulation of bone remodeling via mechanically activated ion channels [microform] : grant: NASA NAG 2-791 & NAG 2-1049, final technical report covering the period from May 1, 1992 - December 31, 1994 / Randall L. Duncan, principal investigator.

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

  • A transient response method for linear coupled substructures [microform] / J.R. Admire and J.A. Brunty.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68660

  • An experimental study of fault propagation in a jet-engine controller [microform] / by Gwan Seung Choi.

    • Text
    • Urbana, IL : Coordinated Science Laboratory, College of Engineering, University of Illinois at Urbana-Champaign ; [Washington, D.C. : National Aeronautics and Space Administration, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69066

  • Estimating short-period dynamics using an extended Kalman filter [microform] / Jeffrey E. Bauer, Dominick Andrisani.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69237

  • Compensation in epitaxial cubic SiC films [microform] / B. Segall ... [et al.].

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Centrifuge impact cratering experiment V [microform] : semi-annual report / Boeing Aerospace Company.

    • Text
    • Seattle, Wash. : Boeing Aerospace Company ; Washington, D.C. : NASA Planetary Geophysics, Office of Space Science, [1984]
    • 1984

  • Design and verification guidelines for vibroacoustic and transient environments.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Component Analysis Branch, Systems Dynamics Laboratory, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS105384

  • Design and verification guidelines for vibroacoustic and transient environments [microform].

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Component Analysis Branch, Systems Dynamics Laboratory, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105384

  • Development of higher-order methods for transient thermal and structural analysis [microform] / Charles J. Camarda and Raphael T. Haftka.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS107966

  • An introduction to transient engine applications using the numerical propulsion system simulation (NPSS) and MATLAB® / Jeffrey C. Chin [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2016.
    • 2016-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67314

  • Dynamic simulation of a wave rotor topped turboshaft engine / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
    • 1997-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73175

  • A transient response method for linear coupled substructures / J.R. Admire and J.A. Brunty.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, December 1989.
    • 1989-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS68660

  • Analysis and sizing for transient thermal heating of insulated aerospace vehicle structures / Max L. Blosser.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32506

  • Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators / Ryan D. May, Sanjay Garg.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40528

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