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Articles

Using forward end-sweep to reduce transonic cantilevered stator losses to improve compressor performance

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Pages 293-307 | Received 04 Aug 2017, Accepted 29 Dec 2017, Published online: 19 Jan 2018

References

  • Benini, E., & Biollo, R. (2007). Aerodynamics of swept and leaned transonic compressor rotors. Applied Energy, 84(10), 1012–1027. doi: 10.1016/j.apenergy.2007.03.003
  • Campobasso M. S., Mattheiss M., & Wenger U. (1999). Complementary use of CFD and experimental measurements to assess the impact of shrouded and cantilevered stators in axial compressors (ASME Paper No. 99-GT-208).
  • Danish, S. N., Khan, S. U., Umer, U., Qureshi, S. R., & Ma, C. (2014). Performance evaluation of tandem bladed centrifugal compressor. Engineering Applications of Computational Fluid Mechanics, 8(3), 382–395. doi: 10.1080/19942060.2014.11015523
  • Denton, J. D., & Xu, L. (1998). The exploitation of three-dimensional flow in turbomachinery design. Proceedings ofthe Institution of Mechanical Engineers, Part C: JournalofMechanical Engineering Science, 213(2), 125–137.
  • Denton J. D. & Xu L. (2002). The effects of lean and sweep on transonic fan performance (ASME Paper No. GT2002-30327).
  • Dong Y.Gallimore S. J., & Hodson H. P. (1986). Three-dimensional flows and loss reduction in axial compressors (ASME Paper No. 86-GT-193).
  • Freeman C. (1985). Effects of tip clearance flow on compressor stability and engine performance (VKI Lecture Series LS-1985-05).
  • Friedrichs, J., Baumgarten, S., Kosyna, G., & Stark, U. (2001). Effect of stator design on stator boundary layer flow in a highly loaded single-stage axial-flow low-speed compressor. Journal of Turbomachinery, 123(3), 483–489. doi: 10.1115/1.1370168
  • Gallimore, S. J., Bolger, J. J., Cumpsty, N. A., Taylor, M. J., Wright, P. I., & Place, J. M. M. (2002a). The use of sweep and dihedral in multistage axial flow compressor blading-part I: University research and methods development. Journal of Turbomachinery, 124(4), 521–532. doi: 10.1115/1.1507333
  • Gallimore, S. J., Bolger, J. J., Cumpsty, N. A., Taylor, M. J., Wright, P. I., & Place, J. M. M. (2002b). The use of sweep and dihedral in multistage axial flow compressor blading-part II: Low and high speed designs and test verification. Journal of Turbomachinery, 124(4), 533–541. doi: 10.1115/1.1507334
  • Gümmer, V., Wenger, U., & Kau, H.-P. (2001). Using sweep and dihedral to control three-dimensional flow in transonic stators of axial compressors. Journal of Turbomachinery, 123(1), 40–48. doi: 10.1115/1.1330268
  • Hah C., Puterbaugh S. L., & Wadia A. R. (1998). Control of shock structure and secondary flow field inside transonic compressor rotors through aerodynamic sweep (ASME Paper No. 98-GT-561).
  • Joslyn, H. D., & Dring, R. P. (1985). Axial compressor stator aerodynamics. Journal of Engineering for Gas Turbines and Power, 107(2), 485–492. doi: 10.1115/1.3239754
  • Krishnababu, S. K., Dawes, W. N., Hodson, H. P., Lock, G. D., Hannis, J., & Whitney, C. (2009). Aerothermal investigations of tip leakage flow in axial flow turbines-part II: Effect of relative casing motion. Journal of Turbomachinery, 131(1), 011007. doi: 10.1115/1.2952378
  • Lange, M., Vogeler, K., Mailach, R., & Gomez, S. E. (2013). An experimental verification of a new design for cantilevered stators with large hub clearances. Journal of Turbomachinery, 135(4), 041022. doi: 10.1115/1.4007612
  • Mahesh K. V. & Pradeep A. M. (2013). Numerical investigation of the effect of moving endwall and tip clearance on the losses in a low speed axial flow compressor cascade (ASME Paper No. GTINDIA2013-3596).
  • Sasaki, T., & Breugelmans, F. (1998). Comparison of sweep and dihedral effects on compressor cascade performance. Journal of Turbomachinery, 120(3), 454–463. doi: 10.1115/1.2841738
  • Schulz, H. D., & Gallus, H. D. (1988). Experimental investigation of the three-dimensional flow in an annular compressor cascade. Journal of Turbomachinery, 110(4), 467–478. doi: 10.1115/1.3262220
  • Si X., Teng J., Qiang X., & Feng J. (2017). Different effects of cantilevered and shrouded stators on axial compressor performance (ASME Paper No. GT2017-63261).
  • Smith, L. H., & Yeh, H. (1963). Sweep and dihedral effects in axial-flow turbomachinery. Journal of Fluids Engineering, 85(3), 401–414.
  • Storer, J. A., & Cumpsty, N. A. (1991). Tip leakage flow in axial compressors. Journal of Turbomachinery, 113(2), 252–259. doi: 10.1115/1.2929095
  • Strazisar, A. J., Wood, J. R., Hathaway, M. D., & Suder, K. L. (1989). Laser anemometer measurements in a transonic axial-flow fan rotor (NASA Technical Paper 2879).
  • Tweedt, D. L., Okiishi, T. H., & Hathaway, M. D. (1986). Stator endwall leading-edge sweep and hub shroud influence on compressor performance. Journal of Turbomachinery, 108(2), 224–232. doi: 10.1115/1.3262041
  • Wadia, A. R., Hah, C., & Rabe, D. (2004). The impact of forward sweep on tip clearance flows in transonic compressors. The 24th international congress of the aeronautical sciences, Yokohama, Japan.
  • Wadia, A. R., Szucs, P. N., & Crall, D. W. (1998). Inner workings of aerodynamic sweep. Journal of Turbomachinery, 120(4), 671–682. doi: 10.1115/1.2841776
  • Wang, Z. (2007). Numerical study of a 3.5-stage axial compressor at on-and off-design conditions. Journal of Aerospace Power, 22(9), 1444–1454.
  • Wang, Y., Chen, W., Wu, C., & Ren, S. (2014). Effects of tip clearance size on the performance and tip leakage vortex in dual-rows counter-rotating compressor. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 229(11), 1953–1965. doi: 10.1177/0954410014562483
  • Weingold, H. D., Neubert, R. J., Behlke, R. F., & Potter, G. E. (1997). Bowed stators: An example of CFD applied to improve multistage compressor efficiency. Journal of Turbomachinery, 119(2), 161–168. doi: 10.1115/1.2841086
  • Yoon, S., Selmeier, R., Cargill, P., & Wood, P. (2015). Effect of the stator hub configuration and stage design parameters on aerodynamic loss in axial compressors. Journal of Turbomachinery, 137(9), 091001. doi: 10.1115/1.4029598