[1] |
Curtis E M, Hodson H P, Banieghbal M R. Development of blade profiles for low-pressure turbine applications[J]. Journal of Turbomachinery,1997,119(3):531−538 doi: 10.1115/1.2841154
|
[2] |
Volino R J. Separated flow measurements on a highly loaded low-pressure turbine airfoil[J]. Journal of Turbomachinery,2010,132(1):011007 doi: 10.1115/1.3104608
|
[3] |
Ning W, He L. Some modelling issues on trailing edge vortex shedding[C]. ASME Paper, 99-GT-183
|
[4] |
Coull J D, Thomas R L, Hodson H P. Velocity distributions for low pressure turbines[J]. Journal of Turbomachinery,2010,132(4):041006 doi: 10.1115/1.3192149
|
[5] |
Nakhchi M E, Naung S W, Rahmati M. DNS of secondary flows over oscillating low-pressure turbine using spectral/hp element method[J]. Internation Journal of Heat and Fluid Flow,2020,86:108684 doi: 10.1016/j.ijheatfluidflow.2020.108684
|
[6] |
朱俊强, 屈骁, 张燕峰, 等. 高负荷低压涡轮内部非定常流动机理及其控制策略研究进展[J]. 推进技术,2017,38(10):2186−2199(in Chinese)
Zhu J Q, Qu X, Zhang Y F, et al. Research progress on unsteady flow mechanism and control strategies of high-lift low pressure turbine[J]. Journal of Propulsion Technology,2017,38(10):2186−2199
|
[7] |
陈华寅, 楚武利, 董杰忠, 等. 端壁造型与附面层抽吸耦合流动控制对压气机叶栅的性能影响[J]. 推进技术,2023,44(2):2203048(in Chinese)
Chen H Y, Chu W L, Dong J Z, et al. Effects of profiled end wall and boundary layer suction coupled flow control on compressor cascade performance[J]. Journal of Propulsion Technology,2023,44(2):2203048
|
[8] |
陆华伟, 任冬智, 孔晓治, 等. 端壁非定常脉冲射流对高速扩压叶栅性能的影响[J]. 推进技术,2023,44(5):67−80(in Chinese)
Lu H W, Ren D Z, Kong X Z, et al. Effects of unsteady end-wall pulsed jets on performance of high speed compressor cascade[J]. Journal of Propulsion Technology,2023,44(5):67−80
|
[9] |
Cortelezzi L, Karagozian A R. On the formation of the counter-rotating vortex pair in transverse jets[J]. Journal of Fluid Mechanics,2001,446:347−373 doi: 10.1017/S0022112001005894
|
[10] |
张鑫, 王勋年. 正弦交流介质阻挡放电等离子体激励器诱导流场研究的进展与展望[J]. 力学学报,2023,55(2):285−298(in Chinese)
Zhang X, Wang X N. Research progress and outlook of flow field created by dielectric barrier discharge plasma actuators driven by a sinusoidal alternating current high-voltage power[J]. Chinese Journal of Theoretical and Applied Mechanics,2023,55(2):285−298
|
[11] |
王钊, 俞建阳, 陈浮. 基于Kriging代理模型的DBD等离子体控制叶顶泄漏流动研究[J]. 工程热物理学报,2020,41(3):573−580(in Chinese)
Wang Z, Yu J Y, Chen F. Numerical investigation based on Kriging surrogate model of tip leakage flow controlled by DBD plasma[J]. Journal of Engineering Thermophysics,2020,41(3):573−580
|
[12] |
Matsunuma T, Segawa T. Tip leakage flow reduction of a linear turbine cascade using string-type DBD plasma actuators[C]. ASME Paper, GT2018-76680
|
[13] |
李国占, 陈浮, 俞建阳, 等. 等离子体气动激励对气膜冷却特性的影响[J]. 工程热物理学报,2018,39(8):1665−1672(in Chinese)
Li G Z, Chen F, Yu J Y, et al. Effects of plasma actuation on film cooling characteristics[J]. Journal of Engineering Thermophysics,2018,39(8):1665−1672
|
[14] |
Pescini E, Suma A, De Giorgi M G, et al. Optimization of plasma actuator excitation waveform and materials for separation control in turbomachinery[J]. Energy Procedia,2017,126:786−793 doi: 10.1016/j.egypro.2017.08.272
|
[15] |
Pescini E, De Giorgi M G, Suma A, et al. Separation control by a microfabricated SDBD plasma actuator for small engine turbine applications: influence of the excitation waveform[J]. Aerospace Science and Technology,2018,76:442−454 doi: 10.1016/j.ast.2018.01.019
|
[16] |
Matsunuma T, Segawa T. Effects of input voltage and freestream velocity on active flow control of passage vortex in a linear turbine cascade using dielectric barrier discharge plasma actuator[J]. Energies,2020,13(3):764 doi: 10.3390/en13030764
|
[17] |
Mahfoze O, Laizet S. Skin-friction drag reduction in a channel flow with streamwise-aligned plasma actuators[J]. International Journal of Heat and Fluid Flow,2017,66(8):83−94
|
[18] |
吴云, 李应红, 朱俊强, 等. 等离子体气动激励抑制压气机叶栅角区流动分离的仿真与实验[J]. 航空动力学报,2009,24(4):830−835(in Chinese)
Wu Y, Li Y G, Zhu J Q, et al. Computational and experimental investigation of plasma aerodynamic actuation based corner flow separation control in a compressor cascade[J]. Journal of Aerospace Power,2009,24(4):830−835
|
[19] |
Li Y H, Wu Y, Zhou M, et al. Control of the corner separation in a compressor cascade by steady and unsteady plasma aerodynamic actuation[J]. Experiments in Fluids,2010,48(6):1015−1023 doi: 10.1007/s00348-009-0787-2
|
[20] |
Shyy W, Jayaraman B, Andersson A. Modeling of glow discharge-induced fluid dynamics[J]. Journal of Applied Physics,2002,92(11):6434−6443 doi: 10.1063/1.1515103
|
[21] |
Stadtmüller P. Investigation of wake-induced transition on the LP turbine cascade T106A-EIZ[C]//DFG- Verbundprojekt Fo 136/11, Version 1.0. Munich, Germany: University of the Armed Forces, 2001
|
[22] |
Wang Y F, Wang F Z, Song Y P, et al. Compressible large eddy simulation of the boundary layer evolution in a low-pressure turbine cascade at different Reynolds numbers[J]. Journal of the Brazilian Society of Mechanical Sciences and Engineering,2021,43(4):222−1-10 doi: 10.1007/s40430-021-02941-6
|