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Transient catalytic combustor modelA quasi-steady gas phase and thermally thin substrate model is used to analyze the transient behavior of catalytic monolith combustors in fuel lean operation. The combustor response delay is due to the substrate thermal inertia. Fast response is favored by thin substrate, short catalytic bed length, high combustor inlet and final temperatures, and small gas channel diameters. The calculated gas and substrate temperature time history at different axial positions provides an understanding of how the catalytic combustor responds to an upstream condition change. The computed results also suggest that the gas residence times in the catalytic bed in the after bed space are correlatable with the nondimensional combustor response time. The model also performs steady state combustion calculations; and the computed steady state emission characteristics show agreement with available experimental data in the range of parameters covered. A catalytic combustor design for automotive gas turbine engine which has reasonably fast response ( 1 second) and can satisfy the emission goals in an acceptable total combustor length is possible.
Document ID
19820005634
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tien, J. S.
(Case Western Reserve Univ. Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-CR-165324
DOE/NASA/3230-1
Report Number: NASA-CR-165324
Report Number: DOE/NASA/3230-1
Accession Number
82N13507
Funding Number(s)
CONTRACT_GRANT: DE-AI01-77CS-51040
CONTRACT_GRANT: NSG-3230
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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