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contributor authorJarrett, Jerome P.
contributor authorGhisu, Tiziano
date accessioned2017-05-09T01:24:44Z
date available2017-05-09T01:24:44Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_09_091008.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159969
description abstractWith limited resources, time spent refining a design is time not spent in selecting its optimal configuration. A multifidelity optimization scheme is applied to the configuration and refinement of a generic core engine compression system. The best designs result from expending between half and three quarters of the total design effort on configuration selection. The performance of the refinement phase is a weak function of the preceding configuration phase when the latter is well into diminishing returns. By exploiting this behavior, the time taken to obtain equally good designs with the same analysis tools and computational resource may be halved.
publisherThe American Society of Mechanical Engineers (ASME)
titleBalancing Configuration and Refinement in the Design of Two Spool Multistage Compression Systems
typeJournal Paper
journal volume137
journal issue9
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4030051
journal fristpage91008
journal lastpage91008
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 009
contenttypeFulltext


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