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Impact of Stagger Angle Nonuniformity on Turbine Aerodynamic Performance
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作者 Weihao Zhang Zhengping Zou +3 位作者 shangneng pan Huoxing Liu Huoxing Liu Wei Li 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第5期465-472,共8页
The assembling error may lead to variation in stagger angles,which would affect the aerodynamic performance of the turbine.To investigate this underlying effect,two parallel numerical experiments on two turbines with ... The assembling error may lead to variation in stagger angles,which would affect the aerodynamic performance of the turbine.To investigate this underlying effect,two parallel numerical experiments on two turbines with the same profile,but uniform and nonuniform vane stagger angle respectively,were conducted in both steady and unsteady methods.The results indicate that certain changes in the detailed flow field of the turbine occur when the stagger angles are nonuniform,further,the blade loading distribution of the vane and rotor become markedly different from that in uniform vane stagger angle situation.Then these consequences caused by nonuniformity mentioned above enhance the unsteadiness of the flow,finally,the aerodynamic performance changes dramatically.It also shows that,compared with steady simulation,the unsteady numerical simulation is necessary in this investigation. 展开更多
关键词 叶片安装角 非均匀性 涡轮机 气动性能 非定常数值模拟 空气动力学性能 配置文件 昼夜温差
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