Dual stability enhancement mechanisms of axial-slot casing treatment in a high-speed mixed-flow compressor with various tip clearances
Tài liệu tham khảo
Brandstetter, 2013, An advanced axial-slot casing treatment on a tip-critical transonic compressor rotor Part 1: Unsteady hot wire and wall pressure measurments
Li, 2018, Effects of the radial blade loading distribution and B parameter on the type of flow instability in a Low-speed axial compressor, Chin J Aeronaut, 31, 1470, 10.1016/j.cja.2018.05.003
Reza, 2015, Alleviation of spike stall in axial compressors utilizing grooved casing treatement, Chin J Aeronaut, 28, 649, 10.1016/j.cja.2015.04.006
Legras, 2010, Numerical analysis of the tip leakage flow field in a transonic axial compressor with circumferential casing treatment, J Therm Sci, 19, 198, 10.1007/s11630-010-0198-y
Ma N, Lin F, Nan X, et al. A numerical investigation of the influence of axial slot casing treatment on tip leakage vortex in an axial compressor. Asian congress on gas turbine; 2014 Aug 19–20; Seoul, Korea. 2014.
Zhou, 2017, Investigation on axial effect of slot casing treatment in a transonic compressor, Applied Thermal Engineering, 2017, 53, 10.1016/j.applthermaleng.2017.07.165
Dong, 2018, Stall margin enhancement of a novel casing treatment subjected to circumferential pressure distortion, Aerosp Sci Technol, 73, 239, 10.1016/j.ast.2017.12.005
Dong, 2014, Experimental investigation on SPS casing treatment with bias flow, Chin J Aeronaut, 27, 1352, 10.1016/j.cja.2014.10.001
Wang, 2017, Experimental and numerical study of tip injection in a subsonic axial flow compressor, Chin J Aeronaut, 30, 907, 10.1016/j.cja.2017.04.004
Li, 2016, Coupling stability-enhancing mechanism with compact self-recirculating injection in an axial flow compressor, J Power Energy, 230, 696, 10.1177/0957650916659778
Hah, 2019, The inner workings of axial casing grooves in a one and a half stage axial compressor with a large rotor tip gap: changes in stall margin and efficiency, Journal of Turbomachinery, 141, 10.1115/1.4041133
Du, 2017
Ross, 2018, Axial compressor stall, circumferential groove casing treatment, and the tip-clearance momentum flux, J Propul Power, 34, 146, 10.2514/1.B36181
Alone, 2017, Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics, Aerosp Sci Technol, 60, 193, 10.1016/j.ast.2016.11.006
Fujita, 1984, A study on configurations of casing treatment for axial flow compressors, Bull JSME, 27, 1675, 10.1299/jsme1958.27.1675
Streit, 2013, An advanced axial-slot casing treatment on a transonic compressor: A close look with computational fluid dynamics and experimental validation, Proc Inst Mech Eng, Part A: J Power Energy, 227, 683, 10.1177/0957650913498736
Streit, 2013
Berdanier, 2018, Effects of tip clearance on stall inception in a multistage compressor, J Propul Power, 34, 308, 10.2514/1.B36364
Lange, 2018, Periodic unsteady tip clearance vortex development in a low-speed axial research compressor at different tip clearances, Journal of Turbomachinery, 140, 10.1115/1.4038319
Sakulkaew, 2013, Compressor efficiency variation with rotor tip gap from vanishing to large clearance, Journal of Turbomachinery, 135, 10.1115/1.4007547
Guinet, 2014
Du, 2008, Numerical simulation on the effect of tip clearance size on unsteadiness in tip clearance flow, J Therm Sci, 17, 337, 10.1007/s11630-008-0337-x
Ciorciari, 2012, Numerical investigation of tip clearance effects in an axial transonic compressor, J Therm Sci, 21, 109, 10.1007/s11630-012-0525-6
Howard, 2017
Hewkin-Smith, 2019, The role of tip leakage flow in spike-type rotating stall inception, Journal of Turbomachinery, 141, 10.1115/1.4042250
Liu, 2016, The stall inceptions in an axial compressor with single circumeferential groove casing treatment at different axial locations, Aerosp Sci Technol, 59, 145, 10.1016/j.ast.2016.10.014
Sun, 2019, Recent development of casing treatments for aero-engine compressors, Chin J Aeronaut, 32, 1, 10.1016/j.cja.2018.11.005
Zhang, 2019, Mechanism investigation of enhancing the stability of an axial flow rotor by blade angle slots, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering [Internet], 10.1177/0954410019829272
Chen, 2014, A computational fluid dynamics study of circumferential groove casing treatment in a transonic axial compressor, Journal of Turbomachinery, 136, 10.1115/1.4024651
Moore, 1977
Cevik, 2016, Casing treatment for desensitization of compressor performance and stability to tip clearance, Journal of Turbomachinery, 138, 10.1115/1.4033420
Rolfes, 2017, Experimental and numerical investigation of a circumferential groove casing treatment in a low speed axial research compressor at different tip clearances, Journal of Turbomachinery, 139, 10.1115/1.4037822
Teichel, 2017, Optimized multidisciplinary design of a small transonic compressor for active high-lift systems, Int J Gas Turb Propul Power Syst, 9, 19, 10.38036/jgpp.9.2_19
Zhang, 2018, Numerical study on flow structures and stall mechanisms on a mixed-flow compressor
Houghton, 2010, Stability enhancement by casing grooves: The importance of stall inception mechanism and solidity, Journal of Turbomachinery, 134, 10.1115/1.4002986
Rajakumar, 2015, Experimental investigations on effects of tip clearance in mixed-flow compressor performance, Proc Inst Mech Eng, Part G: J Aerosp Eng, 229, 933, 10.1177/0954410014541102
Greitzer, 1978, A fundamental criterion for the application of rotor casing treatment, J Fluids Eng, 101, 237, 10.1115/1.3448945
Hembera, 2008, Simulation of casing treatments of a transonic compressor stage, International Journal of Rotating Machinery, 2008, 10.1155/2008/657202
Kim, 2019, Stall inception in low pressure ratio fans, Journal of Turbomachinery, 141, 10.1115/1.4042731
Vo, 2006, Criteria for spike initiated rotating stall, Journal of Turbomachinery, 130, 10.1115/1.2750674
Khalid, 1999, End-wall blockage in axial compressors, J Turbomach, 121, 499, 10.1115/1.2841344