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access icon openaccess Gas–liquid flow field analysis of the compressor vorticity and rotational speed based on NASA Stage 36

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      • 1. Seddigh, F., Saravanamuttoo, H.I.H.: ‘A proposed method for assessing the susceptibility of axial compressors to fouling’, J. Eng. Gas Turbines Power, 1991, 113, (4), pp. 595601.
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      • 2. Mund, F.C., Pilidis, P.: ‘A review of gas turbine online washing systems’. ASME Turbo Expo 2004: Power for Land, Sea, and Air, 2004, pp. 519528.
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      • 3. Reid, L., Moore, R.D.: ‘Design and overall performance of four highly loaded, high speed inlet stages for an advanced high-pressure-ratio core compressor’, (National Aeronautics and Space Administration (NASA), TP-1337, USA, 1978).
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      • 4. Wang, F.J.: ‘The analysis of computational fluid dynamics-the principle and application of the CFD software’ (Tsinghua University Press, Beijing, 2004) (in Chinese).
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      • 5. Bradshaw, P., Cebeci, T., Whitelaw, J.H.: ‘Engineering calculation methods for turbulent flow’ (Academic Press, Salt Lake City, 1981).
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      • 6. Menter, F.R.: ‘Two-equation eddy-viscosity turbulence models for engineering applications’, AIAA J., 1994, 32, (8), pp. 15981605.
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      • 7. Wilcox, D.C.: ‘Reassessment of the scale-determining equation for advanced turbulence models’, AIAA J., 1988, 26, (11), pp. 12991310.
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      • 8. Wu, J.C., Zhenyuan, W.: ‘Elements of vortex aerodynamics’ (Shanghai Jiaotong University Press, Shanghai, 2014) (in Chinese).
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      • 9. Daogan, Y.: ‘Total flow Bernoulli equation in fluid dynamics’, Phys. Eng., 2014, 24, (4), pp. 4753 (In Chinese).
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