참고문헌
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- Wisler, D. C., 1981, "Core Compressor Exit Stage Study, Volume IV : Data and Performance Report for the Best Stage Configuration," NASA CR-165357
- Mailach, R. and Vogeler, K., 2007, "Unsteady Aerodynamic Blade Excitation at the Stability Limit and During Rotating Stall in an Axial Compressor," ASME J. Turbomachinery, Vol. 129, No. 3, pp. 503-511 https://doi.org/10.1115/1.2720486
- Wellborn, S. R. and Okiishi, T. H., 1999, "The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance," ASME J. Turbomachinery, Vol. 121, pp. 486-498 https://doi.org/10.1115/1.2841341
- Camp, T. R. and Day, I. J., 1998, "A Study of Spike and Modal Stall Phenomena in a Low Speed Axial Compressor," ASME J. Turbomachinery, Vol. 120, pp. 393-401 https://doi.org/10.1115/1.2841730
- Fringe, R. and Van Den Braembussche, R., 1984, "Distinction Between Different Types of Impeller and Diffuser Rotating Stall in a Centrifugal Compressor With Vanless Diffuser," ASME J. Turbomachinery, Vol. 106, No. 2, pp. 468-474
피인용 문헌
- vol.12, pp.1, 2009, https://doi.org/10.5293/KFMA.2009.12.1.065