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Experimental evaluation of catalytic combustion with heat removal at near stoichiometric conditions

Author
Bulzan, D. L.
Published
JAN 1, 1980.
Physical Description
1 electronic document
Online Version

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Summary
Two concentric tube configurations were tested. Tests were conducted at an inlet pressure of 150,000 Pa, inlet fuel air mixture temperatures from 780 to 960 K, combustion air flow rates from 0.78 to 1.5 g/s, equivalence ratios up to 0.90, and a range of cooling air flow rates. Propane and propylene fuels were used. Both configurations used air flowing through the center tube for cooling and combustion in the annulus on the catalytic surface. One configuration had the catalyst applied to the outside surface of the inner tube. Conversion of the fuel was very low for this configuration. The other configuration had the catalyst applied to the inside surface of the outer tube. Conversion of the fuel was considerably better in this configuration.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19810015075.
Accession ID: 81N23609.
E-814.
DOE/NASA/51040-23.
NASA-TM-81748.
Workshop on Catalytic Combust.,; 14-15 May 1980; Cincinnati, OH; United States.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15719152