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机译:Effect of loading level and axial distribution on uncertainty performance of turbine blade with geometric variations
School of Energy and Power Engineering, Beihang University, Beijing 100191, China, National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beihang University, Beijing 100191, China;
Research Institute of Aero-Engine, Beihang University, Beijing 100191, China, National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beihang University, Beijing 100191, China;
Turbine blade; Geometric variations; Aerodynamic performance; Uncertainty analysis; Loading; Uncertainty design;