Crystallographic failure analysis of film near cooling hole under temperature gradient of nickel-based single crystal superalloys
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science
Reference10 articles.
1. Three-dimensional flow and heat transfer calculations of film cooling at the leading edge of a symmetrical turbine blade model;Lakehal;International Journal of Heat and Fluid Flow,2001
2. Influence of shaped injection holes on turbine blade leading edge film cooling;Kim;International Journal of Heat and Mass Transfer,2004
3. Three-dimensional flow and heat transfer calculations of film cooling at the leading edge of a symmetrical turbine blade model;Lakehal;International Journal of Heat and Flow,2001
4. High temperature fatigue-creep behaviour of single crystal SRR90 base superalloys: part II-cyclic mechanical response;Li;Fatigue and Fracture of Engineering Materials and Structures,1995
5. Numerical study on elastic–plastic stress field near the cooling holed of nickel-based single crystal air-cooled blades;Yu;Key Engineering Material,2006
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1. The unique influence of 1000 °C high-speed rotation simulated turbine blade working conditions on microstructural degradation of single-crystal superalloy NiAlReRu;Journal of Materials Research and Technology;2024-09
2. Fatigue Assessment of Inclined Film Cooling Holes in Nickel-Based Single-Crystal Superalloy;AIAA Journal;2024-07-14
3. Thermal fatigue failure analysis and life assessment of Ni-based single crystal superalloys with film cooling holes;Engineering Fracture Mechanics;2024-05
4. Effects of Thickness and a Cylindrical Hole on Tensile Behaviors of Nickel-Based Single Crystal Superalloy with Different Secondary Crystal Orientation;2024
5. Gradient Centrifugal Load Driven Microstructural Damage of the Single-Crystal Superalloy Nialreru Components with Flim Cooling Holes at 1000°C;2024
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