机译:Refined flow organization in squealer tip gap and its impact on turbine aerodynamic performance
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beihang University, Beijing 102206. China ,School of Energy & Power Engineering, Beihang University, Beijing 102206, China;
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beihang University, Beijing 102206. China , Research Institute of Aero-engine, Beihang University, Beijing 102206. China;
Turbine; Squealer tip; Leakage flow; Aerodynamic performance; Refined flow organization;