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contributor authorD. R. Sobel
contributor authorL. J. Spadaccini
date accessioned2017-05-08T23:53:28Z
date available2017-05-08T23:53:28Z
date copyrightApril, 1997
date issued1997
identifier issn1528-8919
identifier otherJETPEZ-26764#344_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118688
description abstractStorable 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleHydrocarbon Fuel Cooling Technologies for Advanced Propulsion
typeJournal Paper
journal volume119
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2815581
journal fristpage344
journal lastpage351
identifier eissn0742-4795
keywordsCooling
keywordsFuels
keywordsPropulsion
keywordsCatalysts
keywordsHeat sinks
keywordsFlight
keywordsHeptane
keywordsDesign
keywordsHeat exchangers AND Aircraft
treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002
contenttypeFulltext


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