| [1] Zhang Y F. Investigation of endwall flow behavior and its control strategies in highly-loaded compressor[D]. Xi'an: Northwestern Polytechnical University, 2010. (in Chinese) 张燕峰. 高载荷压气机端壁流动及其控制策略研究[D].西安: 西北工业大学, 2010.[2] Chen P P, Liesner K, Meyer R, et al. Effect of inflow variations on compressor secondary flow behavior[C]//Proceedings of XX Polish Fluid Mechanics Conference, 2012.[3] Liesner K, Meyer R, Schulz S. Non-symmetrical boundary layer suction in a compressor cascade[J]. Journal of Theoretical and Applied Mechanics, 2012, 50(2): 455-472.[4] Hashmi S F A, Qiao W Y, Chen P P. Prediction of hub corner stall characteristics of a highly loaded low speed single stage fan[J]. Journal of Thermal Science, 2011, 20(2): 106-114.[5] Chen P P, Qiao W Y, Hashmi S F A, et al. Passive control of hub-corner separation/stall using axisymmetric-hub contouring[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2012, 226(10): 1214-1224.[6] Costello G R, Cummings R L, Serovy G K. Experimental investigation of axial-flow compressor stator blades designed to obtain high turning by means of boundary-layer suction, NACA-RM-E52D18[R]. Washington, D. C.: NACA, 1952.[7] Sinnettej T, Costello G R. Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines, NACA-TN-2371[R]. Washington, D. C.: NACA, 1951.[8] Peacock R E. Boundary layer suction to eliminate corner separation in cascades of airfoils, NACA-RM-3663[R]. Washington, D. C.: NACA, 1965.[9] Burger G D, Bogardus G. Single-stage evaluation of highly loaded high Mach number compressor stages. 4: Data and performance of hub-slit-suction stator, NASA-CR-120802[R]. Washington, D. C.: NASA, 1971.[10] Kerrebrock J L. Dryden lecture: flow in transonic compressors, AIAA-1980-0124[R]. Reston: AIAA, 1980.[11] Hubrich K, Blcs A, Ott P. Boundary layer suction via a slot in a transonic compressor-numerical parameter study and first experiments, ASME Paper, GT2004-53758 [R]. New York: ASME, 2004.[12] Gbadebo S A, Cumpsty N A, Hynes T P. Control of three dimensional separations in axial compressors by tailored boundary layer suction[J]. Journal of Turbomachinery, 2008, 130(1): 011004.1-011004.8.[13] Gmelin C, Thiele F, Liesner K, et al. Investigations of secondary flow suction in a high speed compressor cascade, ASME Paper, GT2011-46479[R]. New York: ASME, 2011.[14] Lemke M, Gmelin C, Thiele F. Simulations of a compressor cascade with steady secondary flow suction[J]. Numerical Fluid Mechanics and Multidisciplinary Design, 2013, 121: 549-556.[15] Liesner K, Meyer R. Experimental setup for detailed secondary flow investigation by two-dimensional measurement of total pressure loss coefficients in compressor cascades[C]//Proceedings of VKI XIX Symposium on Measurement Techniques in Turbomachinery, 2008.[16] Chen P P, Qiao W Y, Liesner K, et al. Effect of boundary layer suction on compressor hub-corner separation, Part I: Chord-wise and pitch-wise location, ASME Paper, GT2014-25043[R]. New York: ASME, 2014.[17] Lewin E, Koulovic D, Stark U. Experimental and numerical analysis of hub-corner stall in compressor cascades, ASME Paper, GT2010-22704[R]. New York: ASME, 2010.[18] Marciniak V, Kuegeler E, Franke M. Predicting transition on low-pressure turbine profiles[C]//Proceedings of V European Conference on Computational Fluid Dynamics, 2010.[19] Hergt A, Meyer R, Engel K. Experimental investigation of flow control in compressor cascades, ASME Paper, GT2006-90415[R]. New York: ASME, 2006.[20] Gbadebo S A, Cumpsty N A, Hynes T P. Three-dimensional separations in axial compressors[J]. Journal of Turbomachinery, 2005, 127(2): 321-330.[21] Hunt J C R, Wray A A, Moin P. Eddies, streams, and convergence zones in turbulent flows[C]//Studying Turbulence Using Numerical Simulation Databases, 1988: 193-208. |
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