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contributor authorFabio Ciampoli
contributor authorShahrokh Shahpar
contributor authorElisabeth Willocq
contributor authorJohn W. Chew
date accessioned2017-05-09T00:23:43Z
date available2017-05-09T00:23:43Z
date copyrightApril, 2007
date issued2007
identifier issn1528-8919
identifier otherJETPEZ-26949#387_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135735
description abstractThe objective of the research described here is to develop and demonstrate use of automatic design methods for preswirl nozzles. Performance of preswirled cooling air delivery systems depends critically on the design of these nozzles which is subject to manufacturing and stress constraints. The best solution may be a compromise between cost and performance. Here it is shown that automatic optimization using computational fluid dynamics (CFD) to evaluate nozzle performance can be useful in design. A parametric geometric model of a nozzle with appropriate constraints is first defined and the CFD meshing and solution are then automated. The mesh generation is found to be the most delicate task in the whole process. Direct hill climbing (DHC) and response surface model (RSM) optimization methods have been evaluated. For the test case considered, significant nozzle performance improvements were obtained using both methods, but the RSM model was preferred.
publisherThe American Society of Mechanical Engineers (ASME)
titleAutomatic Optimization of Preswirl Nozzle Design
typeJournal Paper
journal volume129
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2364194
journal fristpage387
journal lastpage393
identifier eissn0742-4795
keywordsComputational fluid dynamics
keywordsDesign
keywordsNozzles
keywordsOptimization
keywordsGeometry AND Response surface methodology
treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
contenttypeFulltext


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