High-to-Low Initial Sample Ratio of Hierarchical Kriging for Film Hole Array Optimization
Author:
Affiliation:
1. Seoul National University, Seoul 151-742, Republic of Korea
2. Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea
Funder
Korea Environmental Industry and Technology Institute
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36556
Reference24 articles.
1. Optimization of the Hole Exit Shaping of Film Holes Without and With Compound Angles for Maximal Film Cooling Effectiveness
2. Optimization of a Fan-Shaped Hole for Film Cooling Using a Surrogate Model
3. Film Cooling Hole Shape Optimization Using Proper Orthogonal Decomposition
4. Genetic Algorithm Optimization of a High-Pressure Turbine Vane Pressure Side Film Cooling Array
5. Film Cooling Performance Improvement With Optimized Hole Arrangement on Pressure Side Surface of Nozzle Guide Vane: Part I — Optimization and Numerical Investigation
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