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contributor authorY. Li
contributor authorA. Kirkpatrick
contributor authorC. Mitchell
contributor authorB. Willson
date accessioned2017-05-09T00:13:05Z
date available2017-05-09T00:13:05Z
date copyrightJanuary, 2004
date issued2004
identifier issn1528-8919
identifier otherJETPEZ-26825#192_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130083
description abstractThe topic of this paper is the computational modeling of the gas injection process in a large-bore natural gas fueled engine. At high injection pressures, the overall gas injection and mixing process includes compressible flow features such as rarefaction waves and shock formation. The injection geometries examined in the paper include both a two-dimensional slot and an axisymmetric nozzle. The computations examine the effect of the supply pressure/cylinder stagnation pressure ratio, with ratios ranging from 3 to 80, on the velocity and pressure profiles in the near field region. Computational fluid dynamics modeling was compared with results obtained from a two-dimensional analytical method of characteristics solution and experimental results. The comparison process evaluated factors such as pressure and Mach number profiles, jet boundary shape, and shock location.
publisherThe American Society of Mechanical Engineers (ASME)
titleCharacteristic and Computational Fluid Dynamics Modeling of High-Pressure Gas Jet Injection
typeJournal Paper
journal volume126
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1635398
journal fristpage192
journal lastpage197
identifier eissn0742-4795
keywordsPressure
keywordsHigh pressure (Physics)
keywordsJets
keywordsShock (Mechanics)
keywordsComputational fluid dynamics
keywordsModeling
keywordsNozzles
keywordsComputation
keywordsCylinders
keywordsMach number
keywordsFlow (Dynamics)
keywordsShapes
keywordsEngines
keywordsDisks
keywordsWaves AND Natural gas
treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 001
contenttypeFulltext


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