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contributor authorC. L. Chow
date accessioned2017-05-09T00:57:29Z
date available2017-05-09T00:57:29Z
date copyrightJanuary, 1971
date issued1971
identifier issn1528-8919
identifier otherJETPEZ-26690#13_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151355
description abstractA method of thermal stress and fatigue analysis under triaxial stress conditions is presented. A rotor of a marine steam turbine is taken as a typical example to illustrate the detailed method of analysis in assessing the cycle damage life of the rotor. A computer technique of iterative block relaxation is devised for the thermal stress calculation as the physical geometry of the problem under consideration is fairly complex. This technique is particularly advantageous for such a system as (a) damping the magnitude of the oscillation in the solution of the ill-conditioned stress equations and (b) keeping the number of nodal points required in a converging solution to a minimum. Three different operating procedures of starting and loading the marine turbine have been studied with full three-dimensional stress and fatigue considerations. One of the three procedures which is found to be more desirable is recommended with the descriptions of detailed steam history and main features of the cold start throughout its whole operation.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Stress and Fatigue Analysis in Turbine Rotors
typeJournal Paper
journal volume93
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445384
journal fristpage13
journal lastpage20
identifier eissn0742-4795
keywordsThermal stresses
keywordsRotors
keywordsTurbines
keywordsFatigue analysis
keywordsStress
keywordsGeometry
keywordsSteam
keywordsSteam turbines
keywordsComputers
keywordsCycles
keywordsEquations
keywordsDamping
keywordsOscillations
keywordsFatigue AND Relaxation (Physics)
treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 001
contenttypeFulltext


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