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Airbreathing Pulse Detonation Engine PerformanceThis paper presents performance results for pulse detonation engines taking into account the effects of dissociation and recombination. The amount of sensible heat recovered through recombination in the PDE chamber and exhaust process was found to be significant. These results have an impact on the specific thrust, impulse and fuel consumption of the PDE.
Document ID
20020073120
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Povinelli, Louis A. (NASA Glenn Research Center Cleveland, OH United States)
Yungster, Shaye (Ohio Aerospace Inst. OH United States)
Date Acquired
August 20, 2013
Publication Date
April 1, 2002
Publication Information
Publication: 26th JANNAF Airbreathing Propulsion Subcommittee Meeting
Volume: 1
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20020073093Collected Works26th JANNAF Airbreathing Propulsion Subcommittee Meeting
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