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Displaying 1-19 of 19 results for author "Paxson, Daniel E."
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors [microform] / Daniel E. Paxson.
- 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, 1999]
- 1999
A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system [microform] / Daniel E. Paxson.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
- 1991-1990
A general numerical model for wave rotor analysis [microform] / Daniel E. Paxson.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
An improved numerical model for wave rotor design and analysis [microform] / Daniel E. Paxson and Jack Wilson.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
A comparison between numerically modelled and experimentally measured loss mechanisms in wave rotors [microform] / Daniel E. Paxson.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Recent improvements to and validation of the one dimensional NASA wave rotor model [microform] / Daniel E. Paxson and Jack Wilson.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
A modified through-flow ware rotor cycle with combustor bypass ducts [microform] / Daniel E. Paxson and M. Razi Nalim.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, [1998]
- 1998
Wave augmented diffusers for centrifugal compressors [microform] / Daniel E. Paxson, Gary J. Skoch.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Unsteady ejector performance [microform] : an experimental investigation using a pulsejet driver / Daniel E. Paxson, Jack Wilson and Kevin T. Dougherty.
- 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/LPS30958Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines / Daniel E. Paxson, Thomas A. Kaemming.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo30483Performance 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/gpo31854The influence of unsteadiness on the analysis of pressure gain combustion devices / Daniel E. Paxson, Tom Kaemming.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2013.
- 2013-1
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo51821Numerical 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/gpo57039Using the NASA GRC sectored-one-dimensional combustor simulation / Daniel E. Paxson and Vishal R. Mehta.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
- 2014-3
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo57058Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / Daniel E. Paxson [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2015.
- 2015-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo62842Impact of an exhaust throat on semi-idealized rotating detonation engine performance / Daniel E. Paxson.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016.
- 2016-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo68694Numerical assessment of four-port through-flow wave rotor cycles with passage height variation / D.E. Paxson and Jules W. Lindau.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1997.
- 1997-6
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo79354An incidence loss model for wave rotors with axially aligned passages / Daniel E. Paxson.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1998.
- 1998-6
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo174967An incidence loss model for wave rotors with axially aligned passages / Daniel E. Paxson.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1998.
- 1998-6
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