Investigations on Aerodynamic and Mechanical Performance of Transonic Blade Based on Fluid-Structure Interaction Method
WANG Song-bai1，LI Shao-bin1,2, SONG Xi-zhen1
1. National Key Laboratory of Science and Technology on Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China
In order to research the influence of the fluid-structure interaction for the aerodynamic and mechanical performance of the transonic compressor blade, A time domain two-way fluid-structure interaction numerical method with ANSYS-CFX/Multiphysics was applied to study the aerodynamic performance of transonic blade under aerodynamic and centrifugal forces. The mechanical performance was analyzed by comparing the results between one-way and two-way fluid-structure interaction methods. The results show that the maximum displacement of this blade appears at tip near leading edge, the blade deformation has significant effects on the aerodynamic performance in comparison with the cold blade, which makes passage shock wave position forward and choke mass flow rate increased. Comparing the results between one-way and two-way FSI numerical computation in mechanical performance, the amplitude of the overall blade deformation increases by 1.1%, and the maximum Von-Mises stress increases by 0.8%. The overall results indicate that the industrial practice should adopt a two-way fluid-structure interaction method to guide the aerodynamic design and check the strength, and to improve the safety and reliability of the compressor.
汪松柏1，李绍斌1,2,宋西镇1. 基于流固耦合方法的跨声速叶片气动和强度性能研究[J]. 振动与冲击, 2016, 35(20): 104-110.
WANG Song-bai1，LI Shao-bin1,2, SONG Xi-zhen1. Investigations on Aerodynamic and Mechanical Performance of Transonic Blade Based on Fluid-Structure Interaction Method. JOURNAL OF VIBRATION AND SHOCK, 2016, 35(20): 104-110.
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