《Table 3 Effe cts of improve d nozzle shape on noise and ae rodynamic pe rformance》
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本系列图表出处文件名:随高清版一同展现
《Investigation on Noise Control Technology of Ultra-High Expansion Ratio Turbine》
Effects of improved nozzle shape on noise as w ell as aerodynamic performance of the single stage ultra-high expansion ratio turbine are show n in Table3.The noise level is the average values of the noise at all the observation points in the dow nstream of rotor outlet.As show n in Table 3,the aerodynamic noise w as reduced by more than 10 d B w ith the proposed noise control method.Whilst mass flow rate,expansion ratio and adiabatic efficiency change a little.Relative variations of M ach number at nozzle out and rotor inlet/outlet are less than 5%.It is proved that proposed aerodynamic noise control methods are able to reduce noise level by more than10 d B w ithout remarkable effect on aerodynamic performance in this single stage ultra-high expansion ratio turbine.
图表编号 | XD0024931000 严禁用于非法目的 |
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绘制时间 | 2018.02.01 |
作者 | Xinwu Zhao、Hongyan Huang |
绘制单位 | School of Energy Science and Engineering,Harbin Institute of Technology、School of Energy Science and Engineering,Harbin Institute of Technology |
更多格式 | 高清、无水印(增值服务) |
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