Reliability analysis for low cycle fatigue life of the aeronautical engine turbine disc structure under random environment

Materials Science and Engineering: A

Volumn 395, Issue 1-2, 2005, Pages 218-225

  Liu, C L ^a   Lu, Z Z ^a   Xu, Y L ^b   Yue, Z F ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b CHINA AVIATION POWERPLANT RESEARCH INSTITUTE   (China)

Author keywords

Load life interference model; Low cycle fatigue life; Reliability analysis; Turbine disc

Indexed keywords

AEROSPACE ENGINEERING; COMPUTER SIMULATION; CYCLIC LOADS; FATIGUE OF MATERIALS; PROBABILITY DENSITY FUNCTION; STRAIN; STRESSES;

AERONAUTICAL ENGINE TURBINE DISC STRUCTURES; LINEAR DAMAGE ACCUMULATION (LDA); LOW CYCLE FATIGUE LIFE (LCFL);

MATERIALS SCIENCE;

TURBIDITY;

EID: 14744294468     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.msea.2004.12.014     Document Type: Article

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