Research Catalog

  • Impact of dissociation and sensible heat release on pulse detonation and gas turbine engine performance [microform] / Louis A. Povinelli.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23289
  • A performance map for ideal air breathing pulse detonation engines [microform] / Daniel E. Paxon.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26960
  • Role of air-breathing pulse detonation engines in high speed propulsion [microform] / Louis A. Povinelli, Jin-Ho Lee, Michael O. Anderberg.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26949
  • Innovative airbreathing propulsion concepts for access to space [microform] / Woodrow Whitlow, Richard A. Blech, and Isaiah M. Blankson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27532
  • Effects of fuel distribution on detonation tube performance [microform] / Hugh Douglas Perkins.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
  • Pulse detonation engines for high speed flight [microform] / Louis A. Povinelli.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS51548
  • Thrust augmentation measurements using a pulse detonation engine ejector [microform] / Robert J. Santoro and Sibtosh Pal.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55218
  • Real gas effects on the performance of hydrocarbon-fueled pulse detonation engines [microform] / Louis A. Povinelli, Shaye Yungster.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59493
  • Performance impact of deflagration to detonation transition enhancing obstacles / Daniel E. Paxson, Frederick Schauer and David Hopper.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo31854
  • Numerical analysis of a rotating detonation engine in the relative reference frame / Daniel E. Paxson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57039
  • Pulse detonation engines for high speed flight / Louis A. Povinelli.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2002.
    • 2002-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS51548
  • Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
    • 2002-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS53266

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