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Numerical evaluation of tandem rotor for highly loaded transonic fan 被引量:1
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作者 zhao bin liu bao-jie 《航空动力学报》 EI CAS CSCD 北大核心 2011年第6期1352-1361,共10页
Transonic tandem rotor was designed for highly loaded fan at a corrected tip speed of 381 m/s and another conventional rotor was designed as a baseline to evaluate the loading superiority of tandem rotor with three-di... Transonic tandem rotor was designed for highly loaded fan at a corrected tip speed of 381 m/s and another conventional rotor was designed as a baseline to evaluate the loading superiority of tandem rotor with three-dimensional(3-D) numerical simulation.The aft blade solidity and its impact on total loading level were studied in depth.The result indicates that tandem rotor has potential to achieve higher loading level and attain favorable aerodynamic performance in a wide range of loading coefficient 0.55~0.68,comparing with the conventional rotor which produced a total pressure ratio of 2.0 and loading coefficient of 0.42. 展开更多
关键词 transonic fan tandem rotor highly loaded loading coefficient numerical simulation
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