Experimental assessment of a new combined flow control approach in compressor cascade

Experimental Thermal and Fluid Science - Tập 97 - Trang 313-323 - 2018
Jiaguo Hu1,2, Rugen Wang1, Feng Li3, Tianyu Pan2,4
1School of Aeronautics Engineering, Air Force Engineering University, Xi’an, Shaanxi 710038, China
2School of Energy and Power Engineering, Beihang University, Beijing 100191, China
3Chongqing University of Science & Technology, Chongqing 401331, China
4Collaborative Innovation Center of Advanced Aero-Engine, Beihang University, 37 Xueyuan Road, Beijing 100191, China

Tài liệu tham khảo

W.K. Lord, D.G. MacMartin, T.G. Tillman, Flow control opportunities in gas turbine engines, in: Proceedings of Fluids 2000, AIAA Paper 2000-2234, Denver, CO, USA, 2000. http://doi.org/10.2514/6.2000-2234. Traficante, 2016, Flow separation control on a compressor-stator cascade using plasma actuators and synthetic and continuous jets, J. Aerosp. Eng., 29, 04015056, 10.1061/(ASCE)AS.1943-5525.0000539 Chen, 2013, Experimental study of the impact of hole-type suction on the flow characteristics in a high-load compressor cascade with a clearance, Exp. Therm Fluid Sci., 51, 220, 10.1016/j.expthermflusci.2013.08.001 Ji, 2017, Numerical study for active flow control using dielectric barrier discharge actuators, J. Aerosp. Eng., 30, 04017050, 10.1061/(ASCE)AS.1943-5525.0000764 Varpe, 2015, Benefits of nonaxisymmetric endwall contouring in a compressor cascade with a tip clearance, J. Fluids Eng., 137, 051101, 10.1115/1.4028996 Kumar, 2010, Numerical study of effect of streamwise end wall fences on secondary flow losses in two dimensional turbine rotor cascade, Eng. Appl. Comput. Fluid Mech., 4, 580 A. Pesteil, D. Cellier, O. Domercq, V. Perrot, J.C. Boniface, CREATE: advanced CFD for HPC performance improvement, in: ASME GT2012-68844, 2012. http://doi.org/10.1115/GT2012-68844. A. Hergt, R. Meyer, K. Engel, Experimental investigation of flow control in compressor cascades, in: ASME GT2006-90415, 2006. http://doi.org/10.1115/GT2006-90415. Hergt, 2013, Effects of vortex generator application on the performance of a compressor cascade, J. Turbomach., 135, 021026, 10.1115/1.4006605 Wu, 2016, Mechanism analysis of effects of vortex generator on high-load compressor cascade, J. Propul. Technol., 37, 49 Ramzi, 2011, Numerical study of passive control with slotted blading in highly loaded compressor cascade at low mach number, Int. J. Fluid Mach. Syst., 4, 97, 10.5293/IJFMS.2011.4.1.097 Ramzi, 2013, Passive control via slotted blading in a compressor cascade at stall condition, J. Appl. Fluid Mech., 6, 571 Wu, 2014, Influence of the location of the slot at the outlet on the performance of a highly-loaded diffusion cascade, J. Eng. Therm. Energy Power, 29, 121 Wu, 2013, Effect of slotted blade on performance of high-turning angle compressor cascade, J. Aerosp. Power, 28, 2505 Hu, 2016, Separation control by slot jet in a critically-loaded compressor cascade, Int. J. Turbo Jet Eng J. Hu, R. Wang, R. Li, C. He, Q. Li, Experimental investigation on separation control by slot jet in highly loaded compressor cascade, IMechE Part G: J. Aerosp. Eng. (2017). http://doi.org/10.1177/0954410017703145 (in press). R.V. Chima, Computational modeling of vortex generators for turbomachinery, in: ASME GT2002-30677, 2002. http://doi.org/10.1115/GT2002-30677. Kang, 1993