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- W4288045302 abstract "Compressor is the core component of aero-engines, turbochargers, and industrial gas turbines. The problem of aerodynamic instability threatens the overall compressor performance and even the structural integrity of the entire compression system. During the early stage of compressor instability design, the critical B parameter can provide valuable instructions on the type of instability mode that would occur and the sensitivity of the surge boundary to the system parameters. In this paper, a collection of 30 critical B parameter data were acquired through three different approaches. Also, the acquired data covers a wide range of compressor designs, which is reasonably representative. Based on the data, it is found that the existing estimation methods are only valid for certain compressor designs. Therefore, a new estimation method is proposed with the R-square increased from -0.75 to 0.87. This method correlates the critical B parameter with the specific speed, accounting for the effects of different compressor design features and configurations on the critical B parameter, which offers an effective tool in the preliminary evaluation of compressor instability." @default.
- W4288045302 created "2022-07-27" @default.
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- W4288045302 date "2022-09-01" @default.
- W4288045302 modified "2023-10-16" @default.
- W4288045302 title "A new appraisal of critical B parameter in compressor aerodynamic instability design" @default.
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- W4288045302 doi "https://doi.org/10.1016/j.ast.2022.107780" @default.
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