Xing Yang

Deposition and Aero-Thermal Synergetic Design of Internal Swirl Cooling for a Turbine Blade Leading Edge: GAN-Based Optimization

The leading edge of turbine blades is subjected to extreme thermal loads, exaggerated by continuously increasing turbine inlet temperatures. This challenge has motivated the development of increasingly sophisticated internal cooling architectures. However, such intricate and confined geometries exacerbate particulate...