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Experimental and Computational Investigation of Valve Motion in a Resonant Pulse CombustorThe motion of a passive reed-type valve and a poppet-style valve operating in a small scale, liquid-fueled pulse combustor is investigated experimentally. Valve position and combustion chamber pressure are simultaneously measured using an in-house fabricated optical position probe. The reed valve configuration is found to operate in a self-aspirated mode, generating
significant pressure gain. The poppet valve configuration cannot operate without forced air, and does not generate pressure gain. Both type valves are tested in combustors of multiple lengths. Close examination of the respective valve motions indicate that the reed valve is highly non-linear, with unique attributes that appear essential for self-aspiration. Dynamic models for the motion of each valve are implemented in a computational fluid dynamic (CFD) simulation of the pulse combustor in order to assess if this unique valve motion is critical to successful operation. The results show that it is. The implications of these results are
discussed. The need for active actuation with feedback control, rather than passive valve actuation is highlighted as a critical technology for practical resonant pulse combustors.
Document ID
20230017063
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Daniel E. Paxson
(Glenn Research Center Cleveland, Ohio, United States)
H. Douglas Perkins
(Glenn Research Center Cleveland, Ohio, United States)
Shaye Yungster
(HX5, LLC)
Date Acquired
November 21, 2023
Subject Category
Aircraft Propulsion and Power
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.03.05.04
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Combustion
pressure gain combustion
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