[1]GIANNELIS N F, VIO G A, LEVINSKI O.A review of recent developments in the understanding of transonic shock buffet [J]. Progress in Aerospace Sciences, 2017, 92: 39-84.[J].Progress in Aerospace Sciences, 2017, 92(1):39-84
[2]张伟伟, 高传强, 叶正寅.机翼跨声速抖振研究进展[J].航空学报, 2015, 36(04):1056-75
[3]DOLLING D S.Fifty Years of Shock-WaveBoundary-Layer Interaction Research: What Next?[J].AIAA Journal, 2001, 39(8):1517-31
[4]GAO C, ZHANG W.Transonic aeroelasticity: A new perspective from the fluid mode [J]. Progress in Aerospace Sciences, 2020, 113: 100596.[J].Progress in Aerospace Sciences, 2020, 113(1):100596-100596
[5]LEE B H K.Self-sustained shock oscillations on airfoils at transonic speeds[J].Progress in Aerospace Sciences, 2001, 37(2):147-96
[6]CROUCH J D, GARBARUK A, MAGIDOV D, et al.Origin of transonic buffet on aerofoils [J]. Journal of Fluid Mechanics, 2009, 628: 357-69.[J].Journal of Fluid Mechanics, 2009, 628(1):357-369
[7]GAO C, ZHANG W, YE Z.Numerical study on closed-loop control of transonic buffet suppression by trailing edge flap [J]. Computers & Fluids, 2016, 132: 32-45.[J].Computers & Fluids, 2016, 132(1):32-45
[8]TSUKAMOTO Y, KITAMURA K.Numerical Study of Transonic Buffet on SC(2)-0518 and OAT15A with Vortex Generators[J].AIAA Journal, 2024, 62(8):3052-65
[9]田珊珊, 金亮, 杜兆波, 等.基于鼓包的激波边界层干扰控制研究进展[J].航空学报, 2023, 44(18):37-60
[10]BRUCE P J K, COLLISS S P.Review of research into shock control bumps[J].Shock Waves, 2015, 25(5):451-71
[11]GEOGHEGAN J A, GIANNELIS N F, VIO G A.Parametric Study of Active Shock Control Bumps for Transonic Shock Buffet Alleviation; proceedings of the AIAA Scitech 2020 Forum, F, 2020 [C]. American Institute of Aeronautics and Astronautics.
[12]康伟, 胡仕林, 王彦清.介电弹性薄膜翼型的增升效应机理[J].航空学报, 2023, 44(18):112-23
[13]KANG W, HU S, WANG Y.Lift enhancement mechanism study of the airfoil with a dielectric elastic membrane skin [J]. Journal of Fluids and Structures, 2024, 125: 104083.[J].Journal of Fluids and Structures, 2024, 125(1):1-13
[14]胡仕林, 陈柄宙, 康伟.基于动力学模态分解的柔性膜翼增升机制[J].航空学报, 2025, 46(02):137-49
[15]VISBAL M.Viscous and inviscid interactions of an oblique shock with a flexible panel [J]. Journal of Fluids and Structures, 2014, 48: 27-45.[J].Journal of Fluids and Structures, 2014, 48(1):27-45
[16]BROUWER K R, GOGULAPATI A, MCNAMARA J J.Interplay of Surface Deformation and Shock-Induced Separation in ShockBoundary-Layer Interactions[J].AIAA Journal, 2017, 55(12):4258-73
[17]SHINDE V, MCNAMARA J, GAITONDE D, et al.Transitional shock wave boundary layer interaction over a flexible panel [J]. Journal of Fluids and Structures, 2019, 90: 263-85.[J].Journal of Fluids and Structures, 2019, 90(1):263-285
[18]SHINDE V, MCNAMARA J, GAITONDE D.Control of transitional shock wave boundary layer interaction using structurally constrained surface morphing [J]. Aerospace Science and Technology, 2020, 96: 105545.[J].Aerospace Science and Technology, 2020, 96(1):1-13
[19]SHINDE V J, GAITONDE D V, MCNAMARA J J.Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface[J].AIAA Journal, 2021, 59(3):912-26
[20]REN K, GAO C, ZHOU F, et al.Transonic Buffet Active Control with Local Smart Skin[J].Actuators, 2022, 11(6):155-167
[21]HAMADA A A, MARGHA L, ABDELRAHMAN M M, et al.Dynamic shock wave investigations for an unsteady supersonic flow with a morphing bump over a flat plate[J].Shock Waves, 2025, 35(3):215-33
[22]孟祥一, 戴玉婷, 张育鸣，等.流固耦合翼型跨声速抖振载荷控制与机理分析[J].航空学报, 2026, 1(1):1-13
[23]GEOGHEGAN J A, GIANNELIS N F, VIO G A.A Numerical Study on Transonic Shock Buffet Alleviation Through Oscillating Shock Control Bumps; proceedings of the 2018 AIAA Aerospace Sciences Meeting, F, 2018 [C]. American Institute of Aeronautics and Astronautics.
[24]韦莲旖, 郑冠男, 黄程德, 等.跨声速抖振与翼型蒙皮的耦合作用. 第七届全国流固耦合与非常流体力学学术会议, 中国江苏盐城, 2024 [C].
[25]GREENBLATT D, WILLIAMS D R.Flow Control for Unmanned Air Vehicles[J].Annual Review of Fluid Mechanics, 2022, 54(Volume 54,2022):383-412
[26]WYGNANSKI I.On the need to reassess the design tools for active flow control[J].Progress in Aerospace Sciences, 2024, 146(1):1-13
[27]SIMIRIOTIS N, JODIN G, MAROUF A, et al.Morphing of a supercritical wing by means of trailing edge deformation and vibration at high Reynolds numbers: Experimental and numerical investigation [J]. , .[J].Journal of Fluids and Structures, 2019, 91(1):1-12
[28]ROUAIX C, JIMéNEZ-NAVARRO C, CARVALHO M, et al.Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number [J].[J].Journal of Fluids and Structures, 2023, 123(1):1-13
[29]JIMENEZ-NAVARRO C, T? J B, ROUAIX C, et al.Morphing Effects on the Aerodynamic Performances of a Supercritical Wing’s Prototype in Transonic Flow Conditions [M]//TUOVINEN T, PERIAUX J, KNOERZER D, et al. Advanced Computational Methods and Design for Greener Aviation. Cham; Springer International Publishing. 2024: 159-74.
[30]JACQUIN L, MOLTON P, DECK S, et al.Experimental Study of Shock Oscillation over a Transonic Supercritical Profile[J].AIAA Journal, 2009, 47(9):1985-94
[31]ZHAO Y, DAI Z, TIAN Y, et al.Flow characteristics around airfoils near transonic buffet onset conditions[J].Chinese Journal of Aeronautics, 2020, 33(5):1405-20
[32]TIAN Y, GAO S, LIU P, et al.Transonic buffet control research with two types of shock control bump based on RAE2822 airfoil[J].Chinese Journal of Aeronautics, 2017, 30(5):1681-96
CJA