References
- Joslyn, H. and Dring, R., 1985, "Axial Compressor Stator Aerodynamics," Journal of Engineering of Gas Turbines and Power, Vol. 107, No. 2, pp. 485-493. https://doi.org/10.1115/1.3239754
- Lei, V., Spakovszky, Z. and Greitzer, E., 2008, "A Criterion for Axial Compressor Hub-Corner Stall," Journal of Turbomachinery, Vol. 130, 031006. https://doi.org/10.1115/1.2775492
- Wei, M., Xavier, O., Lipeng, L., Francis, L. and Feng, G., 2011 "Experimental Study of Corner Stall in a Linear Compressor Cascade," Chinese Journal of Aeronautics, Vol. 24, pp. 235-242. https://doi.org/10.1016/S1000-9361(11)60028-9
- Choi, M., Baek, J. H., Oh, S. H. and Ki, D. J., 2008, "Role of Hub-Corner-Separation on Rotating Stall in an Axial Compressor," Trans. Japan Soc. Aero. Space Sco., Vol. 51, No. 172, pp.93-100. https://doi.org/10.2322/tjsass.51.93
- Sasaki, T. and Breugelmans, F., 1998, "Comparison of Sweep and Dihedral Effects on Compressor Cascade Performance," Journal of Turbomachinery, Vol. 120, pp. 454-464. https://doi.org/10.1115/1.2841738
- Gummer, V., Wenger, U. and Kau, H., "Using Sweep and Dihedral to Control Three-Dimensional Flow in Transonic Stators of Axial Compressors," 2001, Journal of Turbomachinery, Vol. 123, pp. 40-48. https://doi.org/10.1115/1.1330268
- Breugelmans, F., Carels, Y. and Demuth, M., 1984, "Influence of Dihedral on the Secondary Flow in a Two-Dimensional Compressor Cascade," ASME Journal of Engineering
- Gallimore, S., Bolger, J., Cumpsty, N., Taylor, M., Wright, P. and Place, J., 2002, "The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading-Part I : University Research and Methods Development," ASME Journal of Turbomachinery, Vol. 124, pp. 521-532. https://doi.org/10.1115/1.1507333
- Weingold, H., Neuber, R., Behlk, R., and Potter, G., 1997, "Bowed Stators: An Example of CFD Applied to Improve Multistage Compressor Efficiency," ASME Journal of Turbomachinery, Vol. 119, pp.161-168. https://doi.org/10.1115/1.2841086
- Fischer, A., 2004, "Performance of Strongly Bowed Stators in a Four-Stage High-Speed compressor," ASME Journal of Turbomachinery, Vol. 126, pp. 333-338. https://doi.org/10.1115/1.1649743
- 최민석, 백제현, 2002, "동익 회전속도 변화에 따른 1단 축류 압축기 선회실속의 특성변화 연구," 유체기계 연구 개발 발표회, pp. 258-263.
- Nicloas Buffaz Isabelle Trebinjac, 2012, "Impact of Tip clearance Size and Rotation Speed on the Surge Onset In a High Pressure Centrifugal Compressor," ASME Paper No. GT2012-68427.
- S. A. Khali, A. S. Khalsa, I. A. Waitz, C. S. Tan, E. M. greitzer, N. A. Cumpsty, J. J. Adamczyk and F. E. Marble, 1999, "Endwall Blockage in Axial Compressor," ASME Journal of Turbomachinery, Vol. 121, pp. 499-509. https://doi.org/10.1115/1.2841344
- K. L. Suder, "Blockage Development in a Transonic, Axial Compressor Rotor," ASME Journal of Turbomachinery, Vol. 120, pp. 465-476.
- Reid, L., and Moore, R., 1978, "Design and Overall Performance of Four Highly Loaded, High-Speed Inlet Stages for and Advanced High-Pressure-Ratio Core Compressor," NASA Report No. TP-1337.
- Moore, R., and Reid, L., 1980, "Performance of Single-Stage Axial-Flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and With Design Pressure Ratio of 2.05," NASA Report No. TP-1659.
- Cumpsty, N. A., 1989, Compressor Aeroydynamics, Unites States.
- ANSYS Inc. 2010, ANSYS CFX 13.0 User's manual.