Research Catalog

  • Orbit transfer rocket engine technology program [microform] ; integrated control and health monitoring capacitive displacement sensor development : final report / by Frank N. Collamore.

    • Text
    • Sacramento, CA : GenCorp, Aerojet, Techsystems ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • Sensor fault detection and diagnosis simulation of a helicopter engine in an intelligent control framework [microform] / Jonathan Litt, Mehmet Kurtkaya, and Ahmet Duyar.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Adelphi, Md.] : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • The design of a turboshaft speed governor using modern control techniques [microform] / by G. De los Reyes and D.R. Goughoe.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, NASA Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986
  • Wave rotor-enhanced gas turbine engines [microform] / Gerard E. Welch, Scott M. Jones, and Daniel E. Paxson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Wide speed range turboshaft study [microform] / Martin D'Angelo.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Forced response testing of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Forced response testing of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor [microform] / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Wave engine topping cycle assessment [microform] / Gerard E. Welch.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • 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
  • Small engine technology. Task 4, Advanced small turboshaft compressor (ASTC) performance and range investigation [microform] / Jeff L. Hansen and Robert A. Delaney.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Neural network-based sensor validation for turboshaft engines [microform] / James C. Moller, Jonathan S. Litt and Ten-Huei Guo.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Model-based fault diagnosis for turboshaft engines [microform] / Michael D. Green and Ahmet Duyar, Jonathan S. Litt.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Simulating a small turboshaft engine in a real-time multiprocessor simulator (RTMPS) environment [microform] / Edward J. Milner and Dale J. Arpasi.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986
  • A real-time, portable, microcomputer-based jet engine simulator [microform] / R. A. Blech, J. F. Soeder, and J. R. Mihaloew.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984
  • Dual clearence squeeze film damper for high load conditions [microform] / David P. Fleming.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984
  • Computational study of the CC3 impeller and vaneless diffuser experiment / Sameer Kulkarni, Timothy A. Beach, Gary J. Skoch.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55298
  • Design concepts for cooled ceramic composite turbine vane / Robert J. Boyle, Ankur H. Parikh, and Vinod K. Nagpal.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57223
  • Forced response testing of anaxi-centrifugal turboshaft engine / A. Karl Owen [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Adelphi, Maryland : U.S. Army Research Laboratory, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69828
  • Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70387
  • 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

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