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dc.contributor.authorLiu, Zhiminen_US
dc.contributor.authorMavris, Dimitri N.en_US
dc.contributor.authorVolovoi, Vitali V.en_US
dc.date.accessioned2005-05-26T14:01:18Z
dc.date.available2005-05-26T14:01:18Z
dc.date.issued2001-06en_US
dc.identifier.urihttp://hdl.handle.net/1853/6308
dc.descriptionPresented at 2001 ASME International Joint Power Generation Conference, New Orleans, LA, June 4-7, 2001.en_US
dc.description.abstractA simplified model for creep life prediction of gas turbine components under varying operating conditions is provided. Re-sponse Surface Equations are used to connect operating condi-tions with nodal creep life that is calculated using nodal stresses and temperatures. Then the accumulation of creep rule is applied to determine total creep life. While the present paper is limited to deterministic examples and creep life only, the methodology is expected to be particularly useful for probabilistic prediction of life where the degradation due to both creep and fatigue is taken into account.en_US
dc.format.extent222081 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.publisherGeorgia Institute of Technologyen_US
dc.relation.ispartofseriesASDL; JPGC-2001-PWR-19163en_US
dc.subjectGas turbine enginesen_US
dc.subjectCreep lifeen_US
dc.titleCreep Life Prediction of Gas Turbine Components under Varying Operating Conditionsen_US
dc.typePaper


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