Assessment of Combustion Modes for Internal Combustion Wave Rotors

dc.contributor.authorNalim, M. Razi
dc.date.accessioned2014-02-25T20:09:01Z
dc.date.available2014-02-25T20:09:01Z
dc.date.issued1999-04
dc.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.en_US
dc.identifier.citationNalim, M. R. (1999). Assessment of combustion modes for internal combustion wave rotors. Journal of engineering for gas turbines and power, 121(2), 265-271.en_US
dc.identifier.urihttps://hdl.handle.net/1805/4021
dc.language.isoen_USen_US
dc.subjectCombustionen_US
dc.subjectWavesen_US
dc.subjectRotorsen_US
dc.titleAssessment of Combustion Modes for Internal Combustion Wave Rotorsen_US
dc.typeArticleen_US
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