Dedekind, MO2007-02-082007-06-072007-02-082007-06-071994Dedekind, MO. 1994. Implementation of creep-fatigue model into finite-element code to assess cooled turbine blade. International journal of pressure vessels and piping, vol 59, 03June, pp 13-190308-0161http://hdl.handle.net/10204/1656http://hdl.handle.net/10204/1656Turbine blades which are designed with airfoil cooling are subject to thermo-mechanical fatigue as well as creep damage. These problems arise due to thermal cycling and high operating temperatures in service. An implementation of fatigue and creep damage models into a finite element code is presented. The implementation was designed to be practical and streamlined, as the damage models used require a minimum of materials testing; and by integrating all the code into an existing finite element package, there is no need to search through or transfer large amounts of output data in order to assess results.462623 bytesapplication/pdfenCopyright: 1994 Elsevier Science LtdFatigue creep damageEngineeringTurbine bladesArticleDedekind, M. (1994). Implementation of creep-fatigue model into finite-element code to assess cooled turbine blade. http://hdl.handle.net/10204/1656Dedekind, MO "Implementation of creep-fatigue model into finite-element code to assess cooled turbine blade." (1994) http://hdl.handle.net/10204/1656Dedekind M. Implementation of creep-fatigue model into finite-element code to assess cooled turbine blade. 1994; http://hdl.handle.net/10204/1656.TY - Article AU - Dedekind, MO AB - Turbine blades which are designed with airfoil cooling are subject to thermo-mechanical fatigue as well as creep damage. These problems arise due to thermal cycling and high operating temperatures in service. An implementation of fatigue and creep damage models into a finite element code is presented. The implementation was designed to be practical and streamlined, as the damage models used require a minimum of materials testing; and by integrating all the code into an existing finite element package, there is no need to search through or transfer large amounts of output data in order to assess results. DA - 1994 DB - ResearchSpace DP - CSIR KW - Fatigue creep damage KW - Engineering KW - Turbine blades LK - https://researchspace.csir.co.za PY - 1994 SM - 0308-0161 T1 - Implementation of creep-fatigue model into finite-element code to assess cooled turbine blade TI - Implementation of creep-fatigue model into finite-element code to assess cooled turbine blade UR - http://hdl.handle.net/10204/1656 ER -