Citation: | Wang Xiansheng, Yang Dangguo, Liu Jun, Zhou Fangqi, Shi Ao. Progress of research on noise induced by compressible flow over cavities[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(3): 1-16. DOI: 10.11729/syltlx20170132 |
[1] |
Shaw L, Clark R, Talmadge D. F-111 generic weapons bay acoustic environment[J]. J Aircraft, 1988, 25(2):147-153. DOI: 10.2514/3.45555
|
[2] |
Rowley C W, Williams D R. Dynamics and control of high-Reynolds-number flow over open cavities[J]. Annu Rev Fluid Mech, 2006, 38(1):251-276. DOI: 10.1146/annurev.fluid.38.050304.092057
|
[3] |
Heller H H, Holmes D G, Covert E E. Flow-induced pressure oscillations in shallow cavities[J]. J Sound Vib, 1971, 18(4):545-553. DOI: 10.1016/0022-460X(71)90105-2
|
[4] |
Stallings R L, Wilcox F J. Experimental cavity pressure distributions at supersonic speeds[R]. NASA TP-2683, 1987.
|
[5] |
Sarohia V. Experimental investigation of oscillations in flows over shallow cavities[J]. AIAA J, 1997, 15(7):984-991. DOI: 10.2514-3.60739/
|
[6] |
Rossiter J E. Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds[R]. Aeronautical Research Council Reports and Memoranda, TR-3438, 1964.
|
[7] |
Tam C K W, Block P J W. On the tones and pressure oscillations induced by flow over rectangular cavities[J]. J Fluid Mech, 1978, 89(2):373-399. DOI: 10.1017/S0022112078002657
|
[8] |
Arunajatesan S, Barone M F, Wagner J L, et al. Joint experimental/computational investigation into the effects of finite width on transonic cavity flow[R]. AIAA 2014-3027, 2014.
|
[9] |
Bres G A, Colonius T. Three-dimensional instabilities in compressible flow over open cavities[J]. J Fluid Mech, 2008, 599:309-339. http://meetings.aps.org/Meeting/DFD05/Event/36492
|
[10] |
Crook S D, Lau T C W, Kelso R M. Three-dimensional flow within shallow, narrow cavities[J]. J Fluid Mech, 2013, 735:587-612. DOI: 10.1017/jfm.2013.519
|
[11] |
Beresh S J, Wagner J L, Demauro E P, et al. Resonance characteristics of transonic flow over a rectangular cavity using pulse-burst PIV[R]. AIAA 2016-1344, 2016.
|
[12] |
Beresh S J, Wagner J L, Casper K M, et al. Spatial distribution of resonance in the velocity field for transonic flow over a rectangular cavity[J]. AIAA J, 2017, 55(7):1-16.
|
[13] |
Beresh S J, Wagner J L, Casper K M. Compressibility effects in the shear layer over a rectangular cavity[J]. J Fluid Mech, 2016, 808:116-152. DOI: 10.1017/jfm.2016.540
|
[14] |
杨党国, 范召林, 李建强, 等.后壁倒角对空腔噪声的抑制效果[J].实验流体力学, 2010, 24(5):22-25. DOI: 10.3969/j.issn.1672-9897.2010.05.005
Yang D G, Fan Z L, Li J Q, et al. Suppression effects of rear-face angle of cavity on its aerodynamics noise[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(5):22-25. DOI: 10.3969/j.issn.1672-9897.2010.05.005
|
[15] |
侯中喜, 夏刚, 秦子增.三维超声速开式空腔振荡特性研究[J].国防科技大学学报, 2004, 26(6):1-4. DOI: 10.3969/j.issn.1001-2486.2004.06.001
Hou Z X, Xia G, Qin Z Z. The numerical analysis of oscillatory characteristics in 3D supersonic open cavity[J]. Journal of National University of Defense Technology, 2004, 26(6):1-4. DOI: 10.3969/j.issn.1001-2486.2004.06.001
|
[16] |
司海清, 马晓晖, 陈都, 等.偏航状态下空腔流动的数值模拟[J].南京航空航天大学学报. 2013, 45(2):191-195. DOI: 10.3969/j.issn.1005-2615.2013.02.006
Si H Q, Ma X H, Chen D, et al. Numerical simulation of cavity flow at different yaw angles[J]. Journal of Nanjing University of Aeronautics and Astronautic, 2013, 45(2):191-195. DOI: 10.3969/j.issn.1005-2615.2013.02.006
|
[17] |
李晓东, 刘婧东, 高军辉.空腔流激振荡发声的数值模拟研究[J].力学学报, 2006, 38(5):599-604. http://d.old.wanfangdata.com.cn/Periodical/lxxb200605004
Li X D, Liu J D, Gao J H. Numerical simulation of flow-induced oscillation and sound generation in a cavity[J]. Chinese Journal of Theoretical and Applied Mechanics, 2006, 38(5):599-604. http://d.old.wanfangdata.com.cn/Periodical/lxxb200605004
|
[18] |
刘俊, 杨党国, 王显圣, 等.湍流边界层厚度对三维空腔流动的影响[J].航空学报, 2016, 37(2):475-483. http://d.old.wanfangdata.com.cn/Periodical/hkxb201602011
Liu J, Yang D G, Wang X S, et al. Effect of turbulent boundary layer thickness on a three-dimensional cavity flow[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(2):475-483. http://d.old.wanfangdata.com.cn/Periodical/hkxb201602011
|
[19] |
Rowley C W, Colonius T, Basu A J On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities[J]. J Fluid Mech, 2002, 455(455):315-346. DOI: 10.1017-S0022112001007534/
|
[20] |
Krishnamurty K. Sound radiation from surface cutouts in high speed flow[D]. California: California Institute of Technology, 1956. http://www.researchgate.net/publication/35133550_Sound_radiation_from_surface_cutouts_in_high_speed_flow
|
[21] |
Wagner J, Beresh S J, Casper K M, et al. Relationship between transonic cavity tones and flowfield dynamics using pulse-burst PIV[R]. AIAA 2016-1345, 2016. http://www.researchgate.net/publication/313844747_Relationship_between_Transonic_Cavity_Tones_and_Flowfield_Dynamics_using_Pulse-Burst_PIV
|
[22] |
Zhang X. Compressible cavity flow oscillation due to shear layer instabilities and pressure feedback[J]. AIAA J, 1995, 33(8):1404-1411. DOI: 10.2514/3.12845
|
[23] |
Forestier N, Jacquin L, Geffroy P. The mixing layer over a deep cavity at high-subsonic speed[J]. J Fluid Mech, 2003, 475(475):101-145. http://adsabs.harvard.edu/abs/2003JFM...475..101F
|
[24] |
Beresh S J, Wagner J L, M P B O, et al. Supersonic flow over a finite-width rectangular cavity[J]. AIAA J, 2015, 53(2):296-310. DOI: 10.2514/1.J053097
|
[25] |
Lada C, Kontis K. Experimental studies of open cavity configurations at transonic speeds with flow control[J]. J Aircraft, 2011, 48(2):719-724. DOI: 10.2514/1.C031174
|
[26] |
Zhang X. Experimental investigation of supersonic flow over two cavities in tandem[J]. AIAA J, 2015, 30(2):1182-1190. http://www.researchgate.net/publication/245423833_Experimental_investigation_of_supersonic_flow_over_two_cavities_in_tandem
|
[27] |
Handa T, Miyachi H, Kakuno H, et al. Generation and propagation of pressure waves in supersonic deep-cavity flows[J]. Exp Fluids., 2012, 53(6):1855-1866. DOI: 10.1007/s00348-012-1400-7
|
[28] |
Zhuang N. Experimental investigation of supersonic cavity flow and their control[J]. Dissertation & Theses-Gradworks, 2007, 44(9):2118-2128. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=CC0214405054
|
[29] |
Zhuang N, Alvi F S, Alkislar M B, et al. Supersonic cavity flows and their control[J]. AIAA J, 2006, 44(9):2118-2128. DOI: 10.2514/1.14879
|
[30] |
Wang M, Freund J B, Lele S K. Computational prediction of flow-generated sound[J]. Annu Rev Fluid Mech, 2006, 38(1):483-512. DOI: 10.1146/annurev.fluid.38.050304.092036
|
[31] |
杨党国, 罗新福, 李建强, 等.来流边界层厚度对开式空腔气动声学特性的影响分析[J].空气动力学学报, 2011, 29(4):486-490. DOI: 10.3969/j.issn.0258-1825.2011.04.015
Yang D G, Luo X F, Li J Q, et al. Analysis of aeroacoustic characteristics in open cavities influenced by boundary-layer thickness[J]. Acta Aerodynamica Sinica, 2011, 29(4):486-490. DOI: 10.3969/j.issn.0258-1825.2011.04.015
|
[32] |
赵小见, 赵磊, 冯峰, 等.某空腔低速流动噪声风洞试验[J].航空学报, 2015, 36(7):2145-2154. http://d.old.wanfangdata.com.cn/Periodical/hkxb201507006
Zhao X J, Zhao L, Feng F, et al. Wind tunnel test into noise induced by low-speed cavity flow[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(7):2145-2154. http://d.old.wanfangdata.com.cn/Periodical/hkxb201507006
|
[33] |
吴继飞, 徐来武, 范召林, 等.开式空腔气动声学特性及其流动控制方法[J].航空学报, 2015, 36(7):2155-2165. http://d.old.wanfangdata.com.cn/Periodical/hkxb201507007
Wu J F, Xu L W, Fan Z L, et al. Aeroacoustic characteristics and flow control method of open cavity flow[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(7):2155-2165. http://d.old.wanfangdata.com.cn/Periodical/hkxb201507007
|
[34] |
Yamouni S, Sipp D, Jacquin L. Interaction between feedback aeroacoustic and acoustic resonance mechanisms in a cavity flow:a global stability analysis[J]. J Fluid Mech, 2013, 717(2):134-165. http://europepmc.org/abstract/MED/23324842
|
[35] |
Fontaine R A, Elliott G S, Austin J M, et al. Very near-nozzle shear-layer turbulence and jet noise[J]. J Fluid Mech, 2015, 770:27-51. DOI: 10.1017/jfm.2015.119
|
[36] |
司海清, 王同光.边界条件对三维空腔流激振荡的影响[J].南京航空航天大学学报, 2006, 38(5):595-599. DOI: 10.3969/j.issn.1005-2615.2006.05.013
Si H Q, Wang T G. Influence of boundary conditions on 3D cavity flow induced oscillations[J]. Nanjing University of Aeroacoustics & Astronautics, 2006, 38(5):595-599. DOI: 10.3969/j.issn.1005-2615.2006.05.013
|
[37] |
Lai H, Luo K H. Acoustic source and near field of three-dimensional compressible flow over an open cavity[R]. AIAA 2005-2805, 2005.
|
[38] |
Chen X X, Sandham N D, Zhang X. Cavity flow noise predictions[R]. University of Southampton Report, AFM-07/05, 2007.
|
[39] |
杨党国, 李建强, 梁锦敏.基于CFD和气动声学理论的空腔自激振荡发声机理[J].空气动力学学报, 2010, 28(6):724-730. DOI: 10.3969/j.issn.0258-1825.2010.06.019
Yang D G, Li J Q, Liang J M, et al. Sound generation induced by self-sustained oscillations inside cavities based on CFD and aeroacoustic theory[J]. Acta Aerodynamica Sinica, 2010, 28(6):724-730. DOI: 10.3969/j.issn.0258-1825.2010.06.019
|
[40] |
Gai S L, Kleine H, Neely A J Supersonic flow over a shallow open rectangular cavity[J]. J Aircraft, 2015, 52(2):609-616. DOI: 10.2514/1.C032781
|
[41] |
杨党国, 祝静, 李建强, 等.跨超声速开式空腔流激振荡模态预估分析[J].空气动力学学报, 2014, 32(3):369-375. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201403016
Yang D G, Zhu J, Li J Q, et al. Prediction and analysis of flow oscillation modes inside open cavities at transonic or supersonic speeds[J]. Acta Aerodynamica Sinica, 2014, 32(3):369-375. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201403016
|
[42] |
万振华, 周林, 孙德军.方腔流致振荡及噪声的数值研究[J].空气动力学学报, 2012, 30(3):291-298. DOI: 10.3969/j.issn.0258-1825.2012.03.003
Wan Z H, Zhou L, Sun D J Numerical investigation of flow induced oscillations and noise in a rectangular cavity[J]. Acta Aerodynamica Sinica, 2012, 30(3):291-298. DOI: 10.3969/j.issn.0258-1825.2012.03.003
|
[43] |
Rockwell D, Naudascher E. Review-self-sustaining oscillations of flow past cavities[J]. J Fluids Eng, 1978, 100(2):152-165. DOI: 10.1115/1.3448624
|
[44] |
Lawson S. Review of numerical simulations for high-speed, turbulent cavity flows[J]. Prog Aerospace Sci, 2011, 47(3):186-216. DOI: 10.1016/j.paerosci.2010.11.002
|
[45] |
Sun Y, Nair A G, Taira K, et al. Numerical simulations of subsonic and transonic open-cavity flows[R]. AIAA 2014-3092, 2014. http://www.researchgate.net/publication/269229214_numerical_simulations_of_subsonic_and_transonic_open-cavity_flows
|
[46] |
杨党国, 范召林, 李建强, 等.弹舱流动特性数值模拟及风洞试验研究[J].空气动力学学报. 2009, 27(3):378-383. DOI: 10.3969/j.issn.0258-1825.2009.03.021
Yang D G, Fan Z L, Li J Q, et al. Studies on flow characteristics of cavity by numerical simulation and wind tunnel test[J]. Acta Aerodynamica Sinica, 2009, 27(3):378-383. DOI: 10.3969/j.issn.0258-1825.2009.03.021
|
[47] |
Ahuja K. Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes[R]. NASA Contractor Report 4653, 1995.
|
[48] |
Schmit R F, Grove J E, Semmelmayer F, et al. Nonlinear feedback mechanisms inside a rectangular cavity[J]. AIAA J, 2014, 52(10):2127-2141. DOI: 10.2514/1.J052804
|
[49] |
Moon S J, Gai S L, Kleine H, et al. Supersonic flow over straight shallow cavities including leading and trailing edge modifications[R]. AIAA 2010-4687, 2010. DOI: 10.2514/6.2010-4687
|
[50] |
Robertson G, Kumar R, Doyle S, et al. Acoustics of a supersonic cavity with a generic store[R]. AIAA 2015-1292, 2015. DOI: 10.2514/6.2015-1292
|
[51] |
Gharib M. Response of the cavity shear layer oscillations to external forcing[J]. AIAA J, 1987, 25(1):43-47. DOI: 10.2514/3.9576
|
[52] |
Daoud M, Naguib A M, Bassioni I, et al. Microphone-array measurements of the floor pressure in a low-speed cavity flow[J]. AIAA J, 2006, 44(9):2018-2023. DOI: 10.2514/1.18129
|
[53] |
Gloerfelt X. Cavity noise[C]. VKI Lecture: Aerodynamic noise from wall bounded flows, Brussels, 2009.
|
[54] |
Chung K. Characteristics of compressible rectangular cavity flows[J]. J Aircraft, 2003, 40(1):137-142. DOI: 10.2514/2.3068
|
[55] |
Baseley J, Pastur L R, Lusseyran F, et al. On the modulating effect of three-dimensional instabilities in open cavity flows[J]. J Fluid Mech, 2014, 759:546-578. DOI: 10.1017/jfm.2014.576
|
[56] |
Baseley J, Pastur L R, Delprat N, et al. Space-time aspects of a three-dimensional multi-modulated open cavity flow[J]. Phys Fluids, 2013, 25(6):64105. DOI: 10.1063/1.4811692
|
[57] |
Tracy M B, Plentovich E B, Hemsch M J, et al. Effects of sweep on cavity flow fields at subsonic and transonic speeds[R]. NASA TM-2012-217577, 2012. https://core.ac.uk/display/10568231
|
[58] |
Vikramaditya N S, Kurian J Nonlinear aspects of supersonic flow past a cavity[J]. Exp Fluids, 2012, 52(6):1389-1399. DOI: 10.1007/s00348-012-1261-0
|
[59] |
Kim H J, Aradag S, Knight R D. Two and three dimensional simulations of supersonic cavity flow[R]. AIAA 2006-2431, 2006. https://www.ixueshu.com/document/914fd23eb580fb6e318947a18e7f9386.html
|
[60] |
Wagner J L, Beresh S J, Casper K M, et al. Experimental investigation of aspect-ratio effects in transonic and subsonic rectangular cavity flows[R]. AIAA 2014-1446, 2014.
|
[61] |
Beresh S J, Wagner J L, Pruett B O M. Particle image velocimetry of a three-dimensional supersonic cavity flow[R]. AIAA 2012-0030, 2012. http://www.researchgate.net/publication/268471908_Particle_Image_Velocimetry_of_a_Three-Dimensional_Supersonic_Cavity_Flow
|
[62] |
Das R, Kim H D, Kurian J Experimental study of supersonic entrainment using a cavity[J]. J Propul Power, 2014, 30(5):1-9. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=JJ0234271949
|
[63] |
Ukeiley L, Sheehan M, Coiffet F, et al. Control of pressure loads in geometrically complex cavities[J]. J Aircraft, 2008, 45(3):1014-1024. DOI: 10.2514/1.33324
|
[64] |
Casper K M, Wagner J L, Beresh S J, et al. Complex geometry effects on subsonic cavity flows[R]. AIAA 2015-1291, 2015. https://www.researchgate.net/publication/306305839_Complex_Geometry_Effects_on_Subsonic_Cavity_Flows
|
[65] |
Casper K M, Wagner J L, Beresh S J, et al. Complex geometry effects on supersonic cavity flows[R]. AIAA 2014-3025, 2014.
|
[66] |
Crafton J, Stanfield S, Rogoshchenkov N, et al. Investigation of Passive Flow Control of Cavity Acoustics Using Dynamic Pressure-Sensitive Paint[R]. AIAA 2017-1178, 2017.
|
[67] |
吴继飞, 徐来武, 范召林, 等.内埋弹舱舱门气动特性研究[J].空气动力学学报, 2012, 30(6):744-748. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201206010
Wu J F, Xu L W, Fan Z L, et al. Investigation on aerodynamic characteristics of internal bay's door[J]. Acta Aerodynamica Sinica, 2012, 30(6):744-748. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201206010
|
[68] |
吴继飞, 徐来武, 范召林, 等.内埋武器舱舱门开闭动态模拟试验技术研究[J].实验流体力学, 2015, 29(4):88-94. http://www.syltlx.com/CN/abstract/abstract10865.shtml
Wu J F, Xu L W, Fan Z L, et al. Investigation on dynamic simulation technology of internal weapon bay's doors opening and closing[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(4):88-94. http://www.syltlx.com/CN/abstract/abstract10865.shtml
|
[69] |
Flora T J, Reeder M F, Lofthouse A, et al. Dynamic store release of ice models from a cavity into Mach 2. 9 Flow[J]. J Aircraft, 2014, 51(6):1-15. DOI: 10.2514/1.C032459
|
[70] |
Merrick J D, Reeder M F. Cavity-store interaction under supersonic freestream conditions[R]. AIAA 2015-3017, 2015. http://www.researchgate.net/publication/299644306_Cavity-Store_Interaction_under_Supersonic_Freestream_Conditions
|
[71] |
吴继飞, 罗新福, 范召林.内埋式弹舱流场特性及武器分离特性改进措施[J].航空学报, 2009, 30(10):1840-1845. DOI: 10.3321/j.issn:1000-6893.2009.10.008
Wu J F, Luo X F, Fan Z L, et al. Flow control method to improve cavity flow and store separation characteristics[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(10):1840-1845. DOI: 10.3321/j.issn:1000-6893.2009.10.008
|
[72] |
Coley C J, Lofthouse A J. Correlation of weapon bay resonance and store unsteady force and moment loading[R]. AIAA 2012-0415, 2012. http://www.researchgate.net/publication/269045805_Correlation_of_Weapon_Bay_Resonance_and_Store_Unsteady_Force_and_Moment_Loading
|
[73] |
Murray N E, Jansen B J, Gui L, et al. Measurements of store separation dynamics[R]. AIAA 2009-105, 2009. http://www.researchgate.net/publication/269061737_measurements_of_store_separation_dynamics
|
[74] |
Bjorge S T, Reeder M F, Subramanian C, et al. Flow around an object projected from a cavity into a supersonic freestream[J]. AIAA J, 2005, 43(7):1465-1475. DOI: 10.2514/1.10943
|
[75] |
Wagner J L, Casper K M, Beresh S J, et al. Experimental investigation of fluid-structure interactions in compressible cavity flows[R]. AIAA 2013-3172, 2013. http://www.researchgate.net/publication/269049382_Experimental_Investigation_of_Fluid-Structure_Interactions_in_Compressible_Cavity_Flows
|
[76] |
Wagner J L, Beresh S J, Casper K M, et al. Simultaneous vibration and acoustic measurements of a store in compressible open cavity flow[R]. AIAA 2013-0228, 2013. http://www.researchgate.net/publication/287096751_Simultaneous_vibration_and_acoustic_measurements_of_a_store_in_compressible_open_cavity_flow
|
[77] |
Wagner J Fluid-structure interactions in compressible cavity flows[J]. Phys Fluids, 2015, 27(6):152-165. DOI: 10.1063/1.4922021
|
[78] |
Barone M, Arunajatesan S. Pressure loading within rectangular cavities with and without a captive store[R]. AIAA 2014-1406, 2014. http://www.researchgate.net/publication/269247720_Pressure_Loading_Within_Rectangular_Cavities_With_and_Without_a_Captive_Store
|
[79] |
王显圣, 杨党国, 刘俊, 等.弹性空腔流致噪声/结构振动特性试验[J].航空学报, 2017, 38(7):120873. http://kns.cnki.net/KCMS/detail/detail.aspx?filename=HKXB201707015&dbname=CJFD&dbcode=CJFQ
Wang X S, Yang D G, Liu J, et al. Test on interactions between aeroacoustic noise and structural vibration in elastic cavity flow[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(7):120873. http://kns.cnki.net/KCMS/detail/detail.aspx?filename=HKXB201707015&dbname=CJFD&dbcode=CJFQ
|
[80] |
Cattafesta L N, Song Q, Williams D R, et al. Active control of flow-induced cavity oscillations[J]. Prog. Aerospace Sci., 2008, 44:479-502. DOI: 10.1016/j.paerosci.2008.07.002
|
[81] |
Cattafesta L N, Williams D R, Rowley C W, et al. Review of active control of flow-induced cavity resonance[R]. AIAA 2003-3567, 2003.
|
[82] |
Cattafesta L. Actuators for Active Flow Control[J]. Annu Rev Fluid Mech, 2011, 43(43):247-272. http://d.old.wanfangdata.com.cn/OAPaper/oai_arXiv.org_1204.2491
|
[83] |
Long D F. Spatial structure of cavity pressure fluctuations at transonic speeds[J]. AIAA J, 2006, 44(9):1983-1992. DOI: 10.2514/1.5236
|
[84] |
Flaherty W, Reedy T M, Elliott G S, et al. Investigation of cavity flow using fast-response pressure-sensitive paint[J]. AIAA J, 2014, 52(11):2462-2470. DOI: 10.2514/1.J052864
|
[85] |
冯强, 张洋, 崔晓春.弹舱对飞翼布局飞机气动特性影响及其控制[J].实验流体力学, 2013, 27(3):31-40. DOI: 10.3969/j.issn.1672-9897.2013.03.006
Feng Q, Zhang Y, Cui X C. Study on the effect of weapons bay on aerodynamic characteristics of flying wing aircraft and its control[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(3):31-40. DOI: 10.3969/j.issn.1672-9897.2013.03.006
|
[86] |
Thiemann C L, Milne G J, Vakili A D. An experimental investigation of supersonic cavity flow control with vertical cylinders[R]. AIAA 2013-3173, 2013. http://www.researchgate.net/publication/269049590_An_Experimental_Investigation_of_Supersonic_Cavity_Flow_Control_with_Vertical_Cylinders
|
[87] |
Illy H, Jacquin L, Geffroy P. Observation on the passive control of flow oscillation over a cavity in a transonic regime by means of a spanwise cylinder[R]. AIAA 2008-3774, 2008.
|
[88] |
Dudley J G, Ukeiley L. Suppression of fluctuating surface pressures in a supersonic cavity flow[R]. AIAA 2010-4974, 2010. http://www.researchgate.net/publication/268483009_Suppression_of_Fluctuating_Surface_Pressures_in_a_Supersonic_Cavity_Flow
|
[89] |
Zhang X, Chen X X, Rona A, et al. Attenuation of cavity flow oscillation through leading edge flow control[J]. J Sound Vib, 1999, 221(1):23-47. DOI: 10.1006/jsvi.1998.2012
|
[90] |
Pereira J C F, Sousa J M M. Influence of impingement edge geometry on cavity flow oscillations[J]. AIAA J, 1994, 32(8):1737-1740. DOI: 10.2514/3.12168
|
[91] |
吴继飞, 陶洋, 范召林, 等.后缘修型对空腔流场特性影响分析[J].空气动力学学报, 2010, 28(2):197-202. DOI: 10.3969/j.issn.0258-1825.2010.02.012
Wu J F, Tao Y, Fan Z L, et al. Analysis of the effect of the modification at the trailing edge on cavity flow characteristics[J]. Acta Aerodynamica Sinica, 2010, 28(2):197-202. DOI: 10.3969/j.issn.0258-1825.2010.02.012
|
[92] |
Gautam T, Lovejeet G, Vaidyanathan A. Experimental study of supersonic flow over cavity with aft Wall offset and cavity floor injection[J]. Aerosp Sci Technol, 2017, 70:211-232. DOI: 10.1016/j.ast.2017.07.024
|
[93] |
Wilcox F J Passive venting system for modifying cavity flowfields at supersonic speeds[J]. AIAA J, 1988, 26(3):374-376. DOI: 10.2514/3.9902
|
[94] |
Stallings R. Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds[R]. NASA Technical Memorandum 4549, 1994.
|
[95] |
Zhang J, Morishita E, Okunuki T, et al. Experimental and computational investigation of supersonic cavity flows[R]. AIAA 2001-1755, 2001. http://www.researchgate.net/publication/269218849_Experimental_and_computational_investigation_of_supersonic_cavity_flows
|
[96] |
Sahoo D, Annaswamy A, Alvi F. Microjets-based active control of store trajectory in a supersonic cavity using a low-order model[R]. AIAA 2005-3097, 2005.
|
[97] |
Sahoo D, Annaswamy A, Zhuang N, et al. Control of cavity tones in supersonic flow[R]. AIAA 2005-793, 2005. DOI: 10.2514/6.2005-793
|
[98] |
Bower W W, Kibens V, Cary A W, et al. High-frequency excitation active flow control for hight-speed weapon release (HIFEX)[R]. AIAA 2004-2513, 2004. http://www.researchgate.net/publication/268561111_High-Frequency_Excitation_Active_Flow_Control_for_High-Speed_Weapon_Release_HIFEX
|
[99] |
George B, Ukeiley L, Cattafesta L N, et al. Control of three-dimensional cavity flow using leading-edge slot blowing[R]. AIAA 2015-1059, 2015. DOI: 10.2514/6.2015-1059
|
[100] |
Thangamani V, Kurian J Control of cavity oscillations in a supersonic flow by microjet injection[J]. J Aircraft, 2013, 50(4):1305-1308. DOI: 10.2514/1.C032003
|
[101] |
王一丁, 郭亮, 童明波, 等.高速飞行器空腔脉动压力主动控制与非线性数值模拟[J].航空学报, 2015, 36(1):213-222. http://d.old.wanfangdata.com.cn/Periodical/hkxb201501017
Wang Y D, Guo L, Tong M B, et al. Active control and nonlinear numerical simulation for oscillating pressure of high-speed aircraft cavity[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):213-222. http://d.old.wanfangdata.com.cn/Periodical/hkxb201501017
|
[102] |
Ali M Y, Solomon J T, Gustavsson J, et al. Control of resonant flow inside a supersonic cavity using high bandwidth pulsed micro-actuators[R]. AIAA 2010-1198, 2010. http://www.researchgate.net/publication/269051079_control_of_resonant_flow_inside_a_supersonic_cavity_using_high_bandwidth_micro-actuators
|
[103] |
吴继飞, 罗新福, 徐来武, 等.活塞式合成射流技术及其应用研究[J].实验流体力学, 2014, 28(6):61-65. http://www.syltlx.com/CN/abstract/abstract10791.shtml
Wu J F, Luo X F, Xu L W, et al. Investigation on piston-typed synthetic jet technology and its application[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(6):61-65. http://www.syltlx.com/CN/abstract/abstract10791.shtml
|
[104] |
罗柏华, 胡章伟, 戴昌晖.声激励抑制空腔流激振荡的实验研究[J].南京航空航天大学学报, 1999, 31(1):1-5. DOI: 10.3969/j.issn.1005-2615.1999.01.001
Luo B H, Hu Z W and Dai C H. Experimental study on suppression of cavity flow oscillations by means of acoustic excitation[J]. Journal of Nanjing University of Aeronautics and Astronautics, 1999, 31(1):1-5. DOI: 10.3969/j.issn.1005-2615.1999.01.001
|
[105] |
Chan S, Zhang X, Gabriel S. The attenuation of cavity tones using plasma actuators[R]. AIAA 2005-2802, 2005. http://www.researchgate.net/publication/268582149_The_Attenuation_of_Cavity_Tones_Using_Plasma_Actuators
|
[106] |
Webb N, Samimy M. Control of supersonic cavity flow using plasma actuators[J]. AIAA, 2017, 55(60):1-10. DOI: 10.2514/1.J055720
|
[107] |
Williams D R, Rowley C W. Recent progress in closed-loop control of cavity tones[R]. AIAA 2006-712, 2006. DOI: 10.2514/6.2006-712
|
[108] |
Williams D R, Cornelius D, Rowley C W. Closed-loop control of linear supersonic cavity tones[R]. AIAA 2007-4226, 2007. http://www.researchgate.net/publication/255583442_Closed-Loop_Control_of_Linear_Supersonic_Cavity_Tones
|
[109] |
Kim K, Debiasi M, Schultz R, et al. Dynamic compensation of a syntheitic jetlike actuator for closed-loop cavity flow control[J]. AIAA J, 2008, 46(1):232-240. DOI: 10.2514/1.30095
|
[110] |
Illingworth S J, Morgans A S, Rowley C W. Feedback control of cavity flow oscillations using simple linear models[J]. J Fluid Mech, 2012, 709(4):223-248. http://www.ams.org/mathscinet-getitem?mr=2989175
|
[111] |
Cattafesta L N, Shukla D, Garg S, et al. Development of an adaptive weapons-bay suppression system[R]. AIAA 1999-1901. 1999. DOI: 10.2514/6.1999-1901
|
[112] |
张征宇, 王显圣, 黄旭辉, 等.高速复杂流动结构的视频测量[J].航空学报, 2017, 38(8):120989. http://d.old.wanfangdata.com.cn/Periodical/hkxb201708003
Zhang Z Y, Wang X S, Huang X H, et al. Videogrammetry measurement for high-speed complex flow structure[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(8):120989. http://d.old.wanfangdata.com.cn/Periodical/hkxb201708003
|
[113] |
周方奇, 杨党国, 王显圣, 等.前缘直板绕流对高速空腔的降噪效果分析[J].航空学报, 2018, 39(6):21812.
Zhou F Q, Yang D G, Wang X S, et al. The effect of leading edge plate on high speed cavity noise controlling[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(6):21812.
|