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Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A018, September 21–25, 2020
Paper No: GT2020-14571
...AERODYNAMIC PERFORMANCE PREDICTION OF TRANSONIC AXIAL MULTISTAGE COMPRESSORS BASED ON ONE-DIMENSIONAL MEANLINE METHOD Yingying Zhang 1,2, Shijie Zhang 1,2, Yunhan Xiao 1,2 1Key Laboratory of Advanced Energy and Power, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing...
Proc. ASME. GT2012, Volume 3: Cycle Innovations; Education; Electric Power; Fans and Blowers; Industrial and Cogeneration, 489-499, June 11–15, 2012
Paper No: GT2012-69987
... properties distribution has been obtained using meanline code combined with a quasi-3D streamline curvature code. Any number of sections from hub to tip of each blade can be used for the determination of the blade shape. The compressor operation map calculated is validated against published test data...
Proc. ASME. GT2012, Volume 8: Turbomachinery, Parts A, B, and C, 2001-2010, June 11–15, 2012
Paper No: GT2012-68577
... is introduced, which allows to firstly improve each of the low-fidelity inputs during high-fidelity optimization and then to converge to the final Pareto-front. The method is applied to a compressor design problem where a low-fidelity 1D meanline code is combined with a higher-fidelity 2D streamline curvature...