Introduction
摘要
This book presents the outcomes of the H2020-MSCA-ITN TEAMAero project, which addresses key aerodynamic challenges in achieving Flightpath 2050 goals for European aviation. Focusing on shock wave boundary layer interactions (SBLI), TEAMAero explores advanced flow control strategies to enhance performance in high-speed, transonic flow environments. Through a multidisciplinary collaboration of universities, research centers, and industry, the project trained 15 researchers and delivered breakthroughs in numerical methods, experimental techniques, and flow-control devices. The findings support the design of more efficient aircraft and engines by improving understanding and control of complex three-dimensional, unsteady transonic flows in both internal and external configurations.