Probabilistic remaining creep life assessment for gas turbine components under varying operating conditions

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 1, Issue , 2002, Pages 587-597

  Liu, Zhimin ^a   Volovoi, Vitali ^a   Mavris, Dimitri N ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CREEP; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; HIGH TEMPERATURE EFFECTS; MATHEMATICAL MODELS; PROBABILITY; STRESSES;

GAS TURBINE COMPONENTS;

GAS TURBINES;

EID: 0036072702     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. The application of the graham and walles creep equation to aeroengine supperalloys
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3. Creep life assessment methods
4. The influence of creep on the fatigue life of nickel base superalloys
5. Numerical analysis of creep components
6. Creep failure assessment of a turbine disc using non-linear finite element method
7. Economic uncertainty assessment using a combined design experiments/Monte Carlo simulation approach with an application to an HSCT