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contributor authorA. Ghafourian
contributor authorM. H. Saidi
contributor authorS. Jahangirian
contributor authorM. Abarham
date accessioned2017-05-09T00:23:41Z
date available2017-05-09T00:23:41Z
date copyrightApril, 2007
date issued2007
identifier issn1528-8919
identifier otherJETPEZ-26949#622_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135721
description abstractA new experimental facility was designed, fabricated, and tested to model and study the effect of bidirectional swirl flow on the rate of heat transfer to combustion chamber walls. Reduction of this heat transfer can result in time and cost of design and fabrication methods of combustion chambers. The experimental study was performed using propane and air with oxygen as fuel and oxidizer, respectively. For similar flow rates, in cases where bidirectional flow was present, wall temperature reductions of up to 70% were observed. In cases where only some of the oxidizer was injected from the chamber end to generate the bidirectional swirl flow, the lowest wall temperature existed. This can be due to better mixing of fuel and oxidizer and absence of hot spots in the combustion core.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Vortex Flow on Heat Transfer to Combustion Chamber Wall
typeJournal Paper
journal volume129
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2431386
journal fristpage622
journal lastpage624
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsHeat transfer
keywordsCombustion
keywordsFuels
keywordsCombustion chambers
keywordsOxygen
keywordsVortex flow AND Wall temperature
treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
contenttypeFulltext


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