Author:
Naseri A.,Boroomand M.,Sammak S.
Publisher
Springer Science and Business Media LLC
Reference29 articles.
1. SAE S-16 Committee. "ARP 1420." Revision B, ”Gas Turbine Inlet Flow Distortion Guidelines,” Society of Automotive Engineers (2002).
2. Sheoran, Y., B. Bouldin, and P. M. Krishnan. “Compressor Performance and Operability in Swirl Distortion.” Journal of Turbomachinery 134, no. 4 (2012): 041008.
3. Fredrick, N., and M. Davis. “Investigation of the Effects of Inlet Swirl on Compressor Performance and Operability Using a Modified Parallel Compressor Model.” In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, Vancouver, Canada, (2011).
4. Nie, Chaoqun, Jingxuan Zhang, Zhiting Tong, and Hongwu Zhang. “The response of a low speed compressor on rotating inlet distortion.” Journal of Thermal Science 15, no. 4 (2006): 314–318.
5. Davis, M., and A. Hale. “A parametric study on the effects of inlet swirl on compression system performance and operability using numerical simulations.” In ASME Turbo Expo 2007: Power for Land, Sea, and Air, pp. 1–10. Montreal, Canada, 2007.
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