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Defining and Measuring Pressure GainThis presentation describes experimental and computational approaches to measuring pressure gain in the various devices currently under investigation wherein the working fluid undergoes a pressure gain combustion (PGC) process. Pressure gain is essentially a measure of the fluid availability for work or thrust production. The devices covered are Resonant Pulse Combustors, Internal Combustion Wave Rotors, Pulse Detonation Engines, and Rotating Detonation Engines. The approaches to pressure gain measurement differ in each device. However, all of the approaches attempt to address the fundamental challenges of PGC system measurement: the extremely harsh environment which makes instrumentation difficult, and the temporal and spatial non-uniformity associated with the exhausting flow which makes assigning a single value to the total pressure difficult. As part of the two-day 2019 International Constant Volume and Detonative Combustion Workshop, held in conjunction with the 2019 AIAA Propulsion and Energy Forum, this presentation is intended to foster discussion and eventual consensus on acceptable measurement methods.
Document ID
20190030506
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Paxson, Dan
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2019
Publication Date
August 17, 2019
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN71983
Meeting Information
Meeting: International Constant Volume Detonation Combustion Workshop
Location: West Lafayette, IN
Country: United States
Start Date: August 17, 2019
End Date: August 18, 2019
Sponsors: Purdue Univ.
Funding Number(s)
WBS: 109492.02.03.02.30
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
pressure gain combustion
detonation
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