NASA NTRS · 20020063440
Airbreathing Pulse Detonation Engine Performance
Abstract
This paper presents performance results for pulse detonation engines (PDE) 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.
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Povinelli, Louis A., Yungster, Shaye. 2002-05-01. Airbreathing Pulse Detonation Engine Performance. https://ntrs.nasa.gov/citations/20020063440
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