Nonlinear continuum damage mechanics model on high temperature creep analysis

Tuijin Jishu/Journal of Propulsion Technology

Volumn 22, Issue 2, 2001, Pages 139-142

  Jing, Jian Ping ^a   Xia, Song Bo ^a   Sun, Yi ^a   Feng, Guo Tai ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Aircraft engine; Creep; Injury; Turbine wheel

Indexed keywords

CONTINUUM MECHANICS; CREEP TESTING; HIGH TEMPERATURE EFFECTS; MATHEMATICAL MODELS; CREEP; GAS TURBINES; MECHANICS;

CONTINUUM DAMAGE MECHANICS; GAS TURBINES DISCS; LINEAR DAMAGE CUMULATING THEORY; CREEP LIFE; GAS TURBINE DISC; NONLINEAR CONTINUUM DAMAGE;

AIRCRAFT ENGINES;

EID: 0035297495     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

1. Troha w, Stabrylla R. Effect of aircraft power usage on turbine engine relative durability and life[R]. AIAA 80-1115.
2. Lemaitre J. Application of damage concepts to predict creep-fatigue failures[J]. Transaction of the ASME, Journal of Engineering Materials and Technology. 1979, 101:284-292.
3. Lemaitre J. How to use damage mechanics[J]. Nuclear Engineering and Design, 1984, 80:233-245.
4. Chaboche J L. Continuum damage mechanics: Part 2[J]. Transaction of the ASME, Journal of Applied Mechanics. 1988, 55(1): 65-72.