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contributor authorY. M. El-Sayed
date accessioned2017-05-08T23:29:48Z
date available2017-05-08T23:29:48Z
date copyrightSeptember, 1989
date issued1989
identifier issn0195-0738
identifier otherJERTD2-26429#111_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105294
description abstractAn optimal thermal design of a considered system configuration is conveniently decided when the system is modeled as made up of one thermodynamic subsystem and of the essential number of design subsystems. The thermodynamic subsystem decides the performance of the components and the design subsystems decide their best matching geometry and costs. An optimizer directs all decisions to an extremum of a given objective function. This decomposition strategy is illustrated by investigating the optimal values of seven decision design variables for a regenerative gas turbine power cycle when a cost-objective function is minimized. The results seen from the point of view of second law analysis and costing are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Decomposition Strategy for Thermoeconomic Optimization
typeJournal Paper
journal volume111
journal issue3
journal titleJournal of Energy Resources Technology
identifier doi10.1115/1.3231412
journal fristpage111
journal lastpage120
identifier eissn1528-8994
keywordsOptimization
keywordsDesign
keywordsGas turbines
keywordsCycles AND Geometry
treeJournal of Energy Resources Technology:;1989:;volume( 111 ):;issue: 003
contenttypeFulltext


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