Show simple item record

contributor authorA. M. Elkady
contributor authorD. M. Kalitan
contributor authorR. Akula
contributor authorH. Karim
contributor authorM. Hadley
contributor authorG. Leonard
contributor authorJ. Herbon
date accessioned2017-05-09T00:50:13Z
date available2017-05-09T00:50:13Z
date copyrightJune, 2012
date issued2012
identifier issn1528-8919
identifier otherJETPEZ-27196#061501_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148813
description abstractIn the present study, a simple perfectly premixed research burner was utilized at temperatures, pressures and residence times representative of an industrial gas turbine cycle to identify the lower limit of NOx and CO emissions, and to establish an emissions benchmark for practical gas turbine combustors. In addition to experimental data, a chemical reactor model has been utilized for the prediction of the NOx and CO, based on detailed chemical reaction mechanisms. Several current kinetics mechanisms were evaluated and subsequently compared to the experimental data. In addition, sensitivity analysis was performed to identify important reactions at the conditions tested, and will be discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleGas Turbine Emission Characteristics in Perfectly Premixed Combustion
typeJournal Paper
journal volume134
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4006058
journal fristpage61501
identifier eissn0742-4795
keywordsCombustion
keywordsCombustion chambers
keywordsGas turbines
keywordsFlames
keywordsTemperature
keywordsEmissions
keywordsMechanisms
keywordsPressure
keywordsChemical kinetics AND Heat losses
treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 006
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record