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    Assessment of Combustion Modes for Internal Combustion Wave Rotors

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002::page 265
    Author:
    M. R. Nalim
    DOI: 10.1115/1.2817116
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Combustion within the channels of a wave rotor is examined as a means of obtaining pressure gain during heat addition in a gas turbine engine. Three modes of combustion are assessed: premixed autoignition (detonation), premixed deflagration, and non-premixed autoignition. The last two will require strong turbulence for completion of combustion in a reasonable time in the wave rotor. The autoignition modes will require inlet temperatures in excess of 800 K for reliable ignition with most hydrocarbon fuels. Examples of combustion mode selection are presented for two engine applications.
    keyword(s): Combustion , Waves , Rotors , Explosions , Fuels , Turbulence , Engines , Channels (Hydraulic engineering) , Pressure , Heat , Temperature , Ignition AND Gas turbines ,
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      Assessment of Combustion Modes for Internal Combustion Wave Rotors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/122151
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. R. Nalim
    date accessioned2017-05-08T23:59:37Z
    date available2017-05-08T23:59:37Z
    date copyrightApril, 1999
    date issued1999
    identifier issn1528-8919
    identifier otherJETPEZ-26788#265_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122151
    description abstractCombustion within the channels of a wave rotor is examined as a means of obtaining pressure gain during heat addition in a gas turbine engine. Three modes of combustion are assessed: premixed autoignition (detonation), premixed deflagration, and non-premixed autoignition. The last two will require strong turbulence for completion of combustion in a reasonable time in the wave rotor. The autoignition modes will require inlet temperatures in excess of 800 K for reliable ignition with most hydrocarbon fuels. Examples of combustion mode selection are presented for two engine applications.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAssessment of Combustion Modes for Internal Combustion Wave Rotors
    typeJournal Paper
    journal volume121
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2817116
    journal fristpage265
    journal lastpage271
    identifier eissn0742-4795
    keywordsCombustion
    keywordsWaves
    keywordsRotors
    keywordsExplosions
    keywordsFuels
    keywordsTurbulence
    keywordsEngines
    keywordsChannels (Hydraulic engineering)
    keywordsPressure
    keywordsHeat
    keywordsTemperature
    keywordsIgnition AND Gas turbines
    treeJournal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 002
    contenttypeFulltext
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