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Roland Mu¨cke
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Proceedings Papers

Coupled Thermo-Mechanical Fatigue Tests for Simulating Load Conditions in Cooled Turbine Parts

Roland Mu¨cke, Klaus Rau
Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 2053-2060, June 6–10, 2011
Paper No: GT2011-45722
DOI: https://doi.org/10.1115/GT2011-45722
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Topics: Fatigue testing, Stress, Thermomechanics, Turbine components, Temperature, Gas turbines, Cooling, Fatigue, Metals, Testing
Proceedings Papers

Probabilistic Finite-Element Analyses on Turbine Blades

Thomas Weiss, Matthias Voigt, Hartmut Schlums, Roland Mu¨cke, Karl-Helmut Becker, Konrad Vogeler
Proc. ASME. GT2009, Volume 6: Structures and Dynamics, Parts A and B, 1093-1102, June 8–12, 2009
Paper No: GT2009-59877
DOI: https://doi.org/10.1115/GT2009-59877
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Topics: Finite element analysis, Turbine blades, Design, Gas turbines, Aircraft engines, Computer simulation, Creep, Crystals, Design methodology, Electricity (Physics)
Proceedings Papers

A Cyclic Life Prediction Approach for Directionally Solidified Nickel Superalloys

Roland Mu¨cke, Piyawan Woratat
Proc. ASME. GT2009, Volume 6: Structures and Dynamics, Parts A and B, 147-155, June 8–12, 2009
Paper No: GT2009-59180
DOI: https://doi.org/10.1115/GT2009-59180
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Topics: Nickel, Superalloys, Anisotropy, Gas turbines, Blades, Creep, Crystals, Failure, Fatigue, Fatigue life
Proceedings Papers

A Viscoplastic Modeling Approach for MCrAlY Protective Coatings for Gas Turbine Applications

Roland Mu¨cke
Proc. ASME. GT2008, Volume 5: Structures and Dynamics, Parts A and B, 195-202, June 9–13, 2008
Paper No: GT2008-50579
DOI: https://doi.org/10.1115/GT2008-50579
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Topics: Gas turbines, Modeling, Protective coatings, Coatings, Oxidation, Stress, Aircraft engines, Computer simulation, Constitutive equations, Corrosion
Proceedings Papers

Non-Local Cyclic Life Prediction for Gas Turbine Components With Sharply Notched Geometries

Roland Mu¨cke, Holger Kiewel
Proc. ASME. GT2007, Volume 5: Turbo Expo 2007, 415-423, May 14–17, 2007
Paper No: GT2007-27448
DOI: https://doi.org/10.1115/GT2007-27448
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Topics: Gas turbines, Stress, Strain gradient, Cooling, Cycles, Design, Failure, Fatigue, Fatigue cracks, Fatigue damage
Proceedings Papers

Probabilistic Lifetime Analysis for Turbine Blades Based on a Combined Direct Monte Carlo and Response Surface Approach

Matthias Voigt, Roland Mu¨cke, Konrad Vogeler, Michael Oevermann
Proc. ASME. GT2004, Volume 6: Turbo Expo 2004, 327-335, June 14–17, 2004
Paper No: GT2004-53439
DOI: https://doi.org/10.1115/GT2004-53439
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Topics: Response surface methodology, Turbine blades, Failure, Probability, Blades, Finite element analysis, Gas turbines, Simulation, Stress