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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
Adobe Acrobat Reader requiredA performance map for ideal air breathing pulse detonation engines [microform] / Daniel E. Paxon.
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[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
Adobe Acrobat Reader requiredRole of air-breathing pulse detonation engines in high speed propulsion [microform] / Louis A. Povinelli, Jin-Ho Lee, Michael O. Anderberg.
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[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
Adobe Acrobat Reader requiredInnovative airbreathing propulsion concepts for access to space [microform] / Woodrow Whitlow, Richard A. Blech, and Isaiah M. Blankson.
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[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
Adobe Acrobat Reader requiredEffects of fuel distribution on detonation tube performance [microform] / Hugh Douglas Perkins.
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[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
2002
0 resources
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/LPS51548Thrust augmentation measurements using a pulse detonation engine ejector [microform] / Robert J. Santoro and Sibtosh Pal.
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[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/LPS55218Real gas effects on the performance of hydrocarbon-fueled pulse detonation engines [microform] / Louis A. Povinelli, Shaye Yungster.
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[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
2003
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS59493Performance impact of deflagration to detonation transition enhancing obstacles / Daniel E. Paxson, Frederick Schauer and David Hopper.
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo31854Numerical analysis of a rotating detonation engine in the relative reference frame / Daniel E. Paxson.
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
2014-3
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo57039Pulse detonation engines for high speed flight / Louis A. Povinelli.
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2002.
2002-9
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS51548Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
2002-10
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS53266