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High-Pressure Turbine Aerodynamic Optimization by 1214051631 is a document available to read on EtoBox.
This study presents an aerodynamic optimization of a high-pressure turbine using a self-adaptive Kriging model, Latin hypercube sampling, and the NSGA-II algorithm to enhance efficiency under varying operational conditions. The optimized blade design achieved a 2.35% increase in isentropic efficiency, primarily influenced by thickness adjustments near the leading edge. The findings also indicate a significant reduction in low-velocity regions and losses, particularly in areas with high entropy generation.
- Author
- 1214051631
- Language
- EN