Storable hydrocarbon fuels that undergo endothermic reaction provide an attractive heat sink for future high-speed aircraft. An investigation was conducted to explore the endothermic potential of practical fuels, with inexpensive and readily available catalysts, under operating conditions simulative of high-speed flight applications. High heat sink capacities and desirable reaction products have been demonstrated for n-heptane and Norpar 12 fuels using zeolite catalysts in coated-tube reactor configurations. The effects of fuel composition and operating condition on extent of fuel conversion, product composition, and the corresponding endotherm have been examined. The results obtained in this study provide a basis for catalytic-reactor/heat-exchanger design and analysis.
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April 1997
Research Papers
Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion
D. R. Sobel,
D. R. Sobel
United Technologies Research Center, East Hartford, CT 06108
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L. J. Spadaccini
L. J. Spadaccini
United Technologies Research Center, East Hartford, CT 06108
Search for other works by this author on:
D. R. Sobel
United Technologies Research Center, East Hartford, CT 06108
L. J. Spadaccini
United Technologies Research Center, East Hartford, CT 06108
J. Eng. Gas Turbines Power. Apr 1997, 119(2): 344-351 (8 pages)
Published Online: April 1, 1997
Article history
Received:
February 15, 1995
Online:
November 19, 2007
Citation
Sobel, D. R., and Spadaccini, L. J. (April 1, 1997). "Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion." ASME. J. Eng. Gas Turbines Power. April 1997; 119(2): 344–351. https://doi.org/10.1115/1.2815581
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