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contributor authorN. L. Sanger
date accessioned2017-05-08T23:15:32Z
date available2017-05-08T23:15:32Z
date copyrightApril, 1983
date issued1983
identifier issn1528-8919
identifier otherJETPEZ-26781#256_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97093
description abstractA method is presented for automating compressor blade design using numerical optimization and is applied to the design of a controlled diffusion stator blade row. A general purpose optimization procedure is employed, which is based on conjugate directions for locally unconstrained problems and on feasible directions for locally constrained problems. Coupled to the optimizer is an analysis package consisting of three analysis programs which calculate blade geometry, inviscid flow, and blade surface boundary layers. The optimization concepts are briefly discussed. Selection of design of a two-dimensional blade section is discussed, and design results are presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading
typeJournal Paper
journal volume105
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227410
journal fristpage256
journal lastpage264
identifier eissn0742-4795
keywordsDesign
keywordsOptimization
keywordsDiffusion (Physics)
keywordsCompressors
keywordsBlades
keywordsGeometry
keywordsStators
keywordsInviscid flow AND Boundary layers
treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002
contenttypeFulltext


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