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contributor authorI. N. Egorov
contributor authorU. I. Babi
contributor authorG. V. Kretinin
contributor authorS. S. Kostiuk
contributor authorI. A. Leshchenko
date accessioned2017-05-09T00:04:45Z
date available2017-05-09T00:04:45Z
date copyrightJuly, 2001
date issued2001
identifier issn1528-8919
identifier otherJETPEZ-26805#495_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125161
description abstractTill now a wide class of aircraft GTE optimization problems has been solved with the help of deterministic approach and it has been quite enough. GTE was considered as ideal system. Strictly speaking, such consideration of any engineering object is incorrect because under the real-life conditions an object is a stochastic system, which has certain indefinites. Therefore the probabilistic estimation of optimization problem results is required.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Methodology of Stochastic Optimization of Parameters and Control Laws for the Aircraft Gas-Turbine Engines Flow Passage Components
typeJournal Paper
journal volume123
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1285841
journal fristpage495
journal lastpage501
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsEngines
keywordsOptimization
keywordsProbability AND Aircraft
treeJournal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 003
contenttypeFulltext


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