Equivalent and simplification of nickel-based single crystal plates with film cooling holes
Author:
Funder
National Natural Science Foundation of China
Natural Science Basic Research Plan in Shaanxi Province of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
1. Forming property and broaching error prediction of a forged nickel-based superalloy turbine disc;Ma;Aerosp. Sci. Technol.,2016
2. A combined CP theory and TCD for predicting fatigue lifetime in single-crystal superalloy plates with film cooling holes;Wen;Int. J. Fatigue,2018
3. Surface slip deformation characteristics for perforated Ni-based single crystal thin plates with square and triangular penetration patterns;Wen;Mater. Sci. Eng. A,2018
4. Numerical and experimental investigation of infrared radiation characteristics of a turbofan engine exhaust system with film cooling central body;Shan;Aerosp. Sci. Technol.,2013
5. Anisotropic creep damage and fracture mechanism of nickel-base single crystal superalloy under multiaxial stress;Wen;J. Alloys Compd.,2017
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1. Fatigue Assessment of Inclined Film Cooling Holes in Nickel-Based Single-Crystal Superalloy;AIAA Journal;2024-07-14
2. Comprehensive evaluation on conjugate heat transfer and thermal stress performance of film cooling;International Journal of Heat and Mass Transfer;2024-02
3. A dislocation-based damage-coupled constitutive model for single crystal superalloy: Unveiling the effect of secondary orientation on creep life of circular hole;International Journal of Plasticity;2024-02
4. Adaptive Positioning Technology of Film Cooling Holes in Hollow Turbine Blades;Aerospace Science and Technology;2024-01
5. Conjugate Heat Transfer and Thermal Stress Characteristics of a Film Cooling Hole in Turbine Vanes;2023
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