Fatigue Assessment of Inclined Film Cooling Holes in Nickel-Based Single-Crystal Superalloy
Author:
Affiliation:
1. Tsinghua University, 100084 Beijing, People’s Republic of China
2. AECC Sichuan Gas Turbine Research Institute, 610500 Chengdu, People’s Republic of China
Abstract
Funder
National Science and Technology Major Projects of China
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J064178
Reference33 articles.
1. Evolution of Ni-based superalloys for single crystal gas turbine blade applications
2. Recent Development in Turbine Blade Film Cooling
3. Three-dimensional flow and heat transfer calculations of film cooling at the leading edge of a symmetrical turbine blade model
4. Crystallographic failure analysis of film near cooling hole under temperature gradient of nickel-based single crystal superalloys
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