A Computational Method of Boundary Layer Blockage inAxial Compressors Based on CFD Results
1.School of Energy and Power Engineering,Dalian University of Technology,Dalian 116024,China;2.Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China
[1] McDougall N M, Cumpsty N A, Hynes T P. Stall Inception in Axial Compressors[J]. Journal of Turbomachinery, 1990, 112(1): 116-123.
[2] Wheeler A P, Miller R J, Hodson H P. The Effect of Wake Induced Structures on Compressor Boundary-Layers[J]. Journal of Turbomachinery, 2007, 129(4): 705-712.
[3] Mellor G L, Wood G M. An Axial Compressor End-Wall Boundary Layer Theory[J]. Journal of Basic Engineering, 1971, 93(2): 300-314.
[4] Hunter I H, Cumpsty N A. Casing Wall Boundary-Layer Development Through an Isolated Compressor Rotor[J]. Journal of Engineering for Power, 1982, 104(4): 805-817.
[5] Rastogi A K, Rodi W. Calculation of General Three-Dimensional Turbulent Boundary Layers[J]. AIAA Journal, 1978, 16(2): 151-159.
[6] Zheng X, Yang H. End-Wall Boundary Layers and Blockages of Multistage Axial Compressors under Different Conditions[J]. Journal of Propulsion & Power, 2016, 33(4): 1-9.
[7] Li Zhi-hui, Zheng Xin-qian, Liu Yan-ming, et al. The Effect of End Wall Boundary Layer on Matching and Corresponding Flow Control Technique for Multistage Axial Compressor[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, 230(12): 2179-2194.
[8] 陈绍文, 孙士珺, 兰云鹤, 等. 来流附面层对吸附式压气机叶栅影响的数值研究[J]. 机械工程学报, 2014, 50(24): 158-163.
[9] Berdanier R A, Key N L. Quantifying Blockage in a Multistage Compressor for Different Tip Clearances Using Steady and Unsteady Pressure Measurements[C]. Boston: 54th AIAA Aerospace Sciences Meeting, 2016.
[10] Suder K L. Blockage Development in a Transonic Axial Compressor Rotor[R]. ASME 1997-GT-394.
[11] Khalid S A, Khalsa A S, Waitz I A, et al. Endwall Blockage in Axial Compressors[J]. Journal of Turbomachinery, 1999, 121(3): 499-509.
[12] Haimes R, Kenwright D. On the Velocity Gradient Tensor and Fluid Feature Extraction[C]. San Diego: 14th Computational Fluid Dynamics Conference, 1999.
[13] Kulkarni S. Development of a Methodology to Estimate Aero-Performance and Aero-Operability Limits of a Multistage Axial Flow Compressor for Use in Preliminary Design[D]. USA: Case Western Reserve University, 2012.
[14] Alfredsson P H, Segalini A, ?rlü R. A New Scaling for the Streamwise Turbulence Intensity in Wall-Bounded Turbulent Flows and What It Tells Us about the “Outer” Peak[J]. Physics of Fluids, 2011, 23(4).
[15] Cliquet J, Houdeville R, Arnal D. Application of Laminar-Turbulent Transition Criteria in Navier-Stokes Computations[J]. AIAA Journal, 2008, 46(5): 1182-1190.
[16] 杨金广, 吴 虎. 改进的Baldwin-Lomax湍流模型及其在叶轮机械中的应用[J]. 工程热物理学报, 2014, 35(3): 451-455.
[17] Drela M. Two-Dimensional Transonic Aerodynamic Design and Analysis Using the Euler Equation[D]. Massachusetts: Massachusetts Institute of Technology, 1985.
[18] Lejon M, Gr?nstedt T, Glodic N, et al. Multidisciplinary Design of a Three Stage High Speed Booster[R]. ASME 2017-GT-64466.
[19] Lakshminarayana B, Suryavamshl N, Prato J, et al. Experimental Investigation of the Flow Field in a Multistage Axial Flow Compressor[R]. ASME 1994-GT-455.