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    Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002::page 344
    Author:
    D. R. Sobel
    ,
    L. J. Spadaccini
    DOI: 10.1115/1.2815581
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: 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.
    keyword(s): Cooling , Fuels , Propulsion , Catalysts , Heat sinks , Flight , Heptane , Design , Heat exchangers AND Aircraft ,
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      Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/118688
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    • Journal of Engineering for Gas Turbines and Power

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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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