The effect of material behaviour on the analysis of single crystal turbine blades: Part II - Component analysis

Fatigue and Fracture of Engineering Materials and Structures

Volumn 25, Issue 4, 2002, Pages 399-409

  Maclachlan, D W ^a,b   Knowles, D M ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

Creep; Fatigue; Finite element simulation; Micromechanism; Single crystal superalloy; Turbine blade component

Indexed keywords

COMPUTER SIMULATION; CREEP; CRYSTAL ORIENTATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; SINGLE CRYSTALS; STRESSES; SUPERALLOYS;

ELASTOVISCOPLASTIC CALCULATIONS; SINGLE CRYSTAL TURBINE BLADE; SLIP SYSTEM MODEL;

TURBOMACHINE BLADES;

EID: 0036537793     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.2002.00505.x     Document Type: Article

References (7)

1. The effect of material behaviour on the analysis of single crystal turbine blades: Part I - Material model
2. Modelling of combined high-temperature creep and cyclic plasticity in components using continuum damage mechanics
3. Constitutive modelling of anisotropic creep deformation in single crystal blade alloys SRR99 and CMSX-4
4. Modelling the uniaxial creep anisotropy of nickel-based single-crystal superalloys CMSX-4 and RR2000 at 1023 K using a slip system-based finite element approach
5. Modelling and predicting the stress rupture properties of single crystal superalloys
6. Fatigue behaviour and lifing of two single-crystal superalloys
7. An assessment of three creep-fatigue life prediction methods for nickel-based superalloy GH4049