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Impact of Dissociation and Sensible Heat Release on Pulse Detonation and Gas Turbine Engine PerformanceA thermodynamic cycle analysis of the effect of sensible heat release on the relative performance of pulse detonation and gas turbine engines is presented. Dissociation losses in the PDE (Pulse Detonation Engine) are found to cause a substantial decrease in engine performance parameters.
Document ID
20010093212
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Povinelli, Louis A. (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2001-211080
NAS 1.15:211080
E-12919
ISABE-2001-1212
Meeting Information
Meeting: 15th International Symposium on Airbreathing Engines
Location: Bangalore
Country: India
Start Date: September 2, 2001
End Date: September 7, 2001
Sponsors: International Society for Airbreathing Engines
Funding Number(s)
PROJECT: RTOP 706-31-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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