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contributor authorM. L. Adams
contributor authorJ. Padovan
contributor authorD. G. Fertis
date accessioned2017-05-08T23:13:11Z
date available2017-05-08T23:13:11Z
date copyrightJuly, 1982
date issued1982
identifier issn1528-8919
identifier otherJETPEZ-26776#586_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95760
description abstractThere is currently a considerable interest and level of activity in developing computational schemes to predict general engine dynamic behavior. The general feeling among researchers working on engine vibration problems is that various modes of operation, such as blade-loss events, require a high level of analysis sophistication to realistically model the engine. Proper account of system nonlinearities (particularly at the bearings, dampers and rubs) appears to be necessary if analytical predictions are to be realistic. The approach described in this paper seeks to make use of already proven general finite-element nonlinear time-transient computer codes which are available on the open market. The work specifically described in this paper covers the first phase of a three-phase NASA-Lewis-sponsored research grant on engine dynamic simulation with available finite element codes. The first phase was concentrated on the development of a bearing-damper element computer software package suitable for “plug-in” to available finite element codes.
publisherThe American Society of Mechanical Engineers (ASME)
titleEngine Dynamic Analysis With General Nonlinear Finite-Element Codes, Part 1: Overall Approach and Development of Bearing Damper Element
typeJournal Paper
journal volume104
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227320
journal fristpage586
journal lastpage593
identifier eissn0742-4795
keywordsBearings
keywordsDampers
keywordsDynamic analysis
keywordsFinite element analysis
keywordsEngines
keywordsSimulation
keywordsVibration
keywordsComputers
keywordsBlades AND Computer software
treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003
contenttypeFulltext


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