风洞试验模型振动机理及主动控制研究进展

doi:10.7527/S1000-6893.2024.30467

本期目录 | 过刊浏览 | 高级检索

| 后一篇

风洞试验模型振动机理及主动控制研究进展

寇西平¹,曾开春¹,马涛¹,路波¹,杨智春²

1. 中国空气动力研究与发展中心
2. 西北工业大学

收稿日期:2024-04-01 修回日期:2024-07-03 出版日期:2024-07-11 发布日期:2024-07-11
通讯作者: 杨智春
基金资助:
智强基金

A Review of Model Vibration Mechanism and Active Control in Wind Tunnel Test

Received:2024-04-01 Revised:2024-07-03 Online:2024-07-11 Published:2024-07-11

摘要/Abstract

摘要： 风洞常规测力试验中经常会出现模型大幅度振动的问题，影响试验数据精度甚至威胁设备安全。深入认识模型振动的发生机理，结合有效的控制手段减小试验中的模型振动幅值，对风洞试验研究有重要意义。首先介绍了风洞模型振动的危害与减小模型振动的意义，分析了模型发生振动的机理，总结了常见的减小模型振动的方法及其研究进展，重点分析了主动振动控制方法涉及的内容与技术难点。已有的研究工作表明，在各种减缓模型振动的方法中，以压电堆作为作动器的主动控制方法最能符合工程实用要求，且减振效果较好。最后对大型风洞中模型振动控制需要研究的问题给出了若干建议。

关键词: 模型振动, 振动主动控制, 压电堆作动器, 控制算法, 风洞试验

Abstract: Undesirable model vibration often occurs in a conventional wind tunnel force test. Large amplitude model vibrations may affect test data adversely and even threaten the safe operation of equipment. It is of great importance to fully understand the mechanism of model vibration occurrence and reduce the vibration amplitude by effective means in wind tunnel tests. The harms of model vibration are introduced at first. Then the types of model vibrations are summarized. The status and progress of reducing model vibrations by various methods are presented. The key points and technical difficulties involved in the active control method are analyzed. The existing literature shows that the active control method with the piezoelectric stack as the actuator can best meet the requirements of the engineering practice, and the vibration damping effect is better than other methods. Finally, several suggestions regarding future research of model vibration control in the large-scale wind tunnel are also presented.

Key words: model vibration, active vibration control, piezoelectric stack actuator, control algorithm, wind tunnel test

中图分类号:

V215.3

寇西平曾开春马涛路波杨智春. 风洞试验模型振动机理及主动控制研究进展[J]. 航空学报, doi: 10.7527/S1000-6893.2024.30467.

参考文献

[1]王发祥.高速风洞试验[M]. 北京: 国防工业出版社, 2003: 1-1.
[2]WANG F X.High speed wind tunnel test[M]. Beijing: National Defence Industry Press, 2003: 1-1 (in Chinese).
[3]MABEY D G, Welsh B L, Pyne C R.A review of rigid body response on sting supported models at high angles of incidence[J].Progress in Aerospace Sciences, 1991, 28(7):133-170
[4]HARALD Q, WOLFGANG S.Assessing model dynamics within the critical alpha range[C]// 52nd Aero-space Sciences Meeting. National Harbor, Maryland: AIAA SciTech Forum, 2014:1484–1496.
[5]郭旭，赵岩.大型风洞设计建设中的结构力学问题[J].中国科学基金, 2017, 5(9):432-437
[6]GUO X, ZHAO Y.Structure mechanics problems in the large scale wind tunnel design and building[J].Bulletin of National Natural Science Foundation of China, 2017, 5(9):432-437
[7]YOUNG J C, POPERNACK J T, GLOSS B.National transonic facility model and model support vi-bration problems[C]//16th Aerodynamic Ground Testing Conference. Seattle, WA: AIAA, 1990: 1416–1425.
[8]KILGORE W A, BALAKRISHNA S, BUTLER D H.Reduction of Tunnel Dynamics at the National Tran-sonic Facility[C]//39nd AIAA Aerospace Sciences Meet-ing and Exhibit. Reno, Nevada: AIAA, 2001: 1162-1174.
[9]PARKER R.Resonance Effects in Wake Shedding from Parallel Plates: Calculation of Resonant Frequencies[J].Journal of Sound and Vibration, 1967, 5(2):330-343
[10]EDWARDS J W.National Transonic Facility Model and Tunnel Vibrations[J].Journal of Aircraft, 2009, 46(1):46-53
[11]PIETER H F，JOOST W K.Stall flutter of sting-supported wind tunnel models[C]//24th AIAA Aerody-namic measurement technology and ground testing con-ference. Portland, Oregon: AIAA, 2004: 2198-2215.
[12]RIVERS M B, BALAKRISHNA S.NASA common research model test envelope extension with active sting damping at NTF[C]//32nd AIAA Applied Aerodynamic Conference. Atlanta, GA: AIAA Aviation, 2014: 3135-3148.
[13]李山青, 刘正兴, 杨耀文.压电材料在智能结构形状和振动控制中的应用[J].力学进展, 1999, 29(1):66-76
[14]LI S Q, LIU Z X, YANG Y W.The applications of pie-zoelectric materials on shape control and vibration control of smart structures[J].[J].Advances in mechanics., 1999,, 29(1):66-76
[15]梁鉴, 张卫国, 王勋年, 等.风洞无人机模型振动抑制系统研制[J].实验流体力学, 2007, 21(4):65-70
[16]LIANG J, ZHANG W G, WANG X N, et al.Develop-ment for restraining oscillation device of the UAV model in the 4m×3m wind tunnel[J].Journal of experiments in fluid mechanics, 2007, 21(4):65-70
[17]路波, 寇西平, 曾开春, 等.风洞常规试验模型尾支杆减振装置: ZL201821445672.3[P]. 2018-09-04.
[18]LU B, KOU X P, ZENG k c, et al.Wind tunnel test model tail sting vibration damping device: China. ZL201821445672.3 [P]. 2018-09-04(in Chinese).
[19]?ur?i? D, Samard?i? M, Marinkovski D, et al.Model sting support with hard metal core for measurement in the blowdown pressurized wind tunnel[J].[J].Measurement,, 2016,, 79(1):130-136
[20]赖志伟, 王成勇, 郑李娟, 等.硬质合金激光加工研究进展[J].硬质合金, 2022, 39(5):335-349
[21]LAI Z W, WANG C Y, ZHENG L J, et al.Research progress on laser processing of cemented carbide[J].Cemented carbide, 2022, 39(5):335-349
[22]刘光远.蜂窝结构支杆测试验证试验[R]. 绵阳: 中国空气动力研究与发展中心, 2022.
[23]LIU G Y.Verification test on honeycomb structure sting [R]. Sichuan, China: China aerodynamics research and development center, 2022(in Chinese).
[24]GLAESE R, BALES G, HSU S, et al.Reduction of dynamic response of a wind tunnel sting mount using a hub damper unit[C]//48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aero-space Exposition, Orlando, Florida: AIAA, 2010: 1307-1316.
[25]HSU S, MOR Marat, STIRLING Bob, et al.Reduction of Dynamic Response of a Wind Tunnel Sting Mount Using Co-cured Composite and Viscoelastic Materi-als[C]//48th AIAA Aerospace Sciences Meeting Includ-ing the New Horizons Forum and Aerospace Exposition, Orlando, Florida: AIAA, 2010: 1308-1316.
[26]PAN J H, LIU Z Q, KOU X P, et al.Constrained layer damping treatment of a model support sting[J].Chinese Journal of Aeronautics, 2020, 24(7):463-469
[27]常冠军.粘弹性阻尼材料[M]. 北京：国防工业出版社, 2012:8-8.
[28]CHANG G J.Viscoelastic damping materials[M]. Bei-jing: National Defence Industry Press, 2012: 8-8 (in Chinese).
[29]WILLIAN B I, FRANCIS J C.Reduction of wind-tunnel-model vibration by means of a tuned damped vi-bration absorber installed in the model: NASA TM X-1606[R]. Hampton, VA: Langley Research Center, 1968.
[30]MABEY D G, ASHILL P R, WELSH B L.Aeroelastic oscillations caused by transitional boundary layers and their attenuation[J].Journal of Aircraft, 1987, 24(7):463-469
[31]陈卫东, 邵敏强, 杨兴华, 等.跨声速风洞测力模型主动减振系统的试验研究[J].振动工程学报, 2007, 20(1):91-97
[32]CHEN W D, SHAO M Q, YANG X H, et al.Experi-mental evaluation of an active vibration control system for wind tunnel aerodynamic models[J].Journal of vibra-tion engineering, 2007, 20(1):91-97
[33]邵敏强.复杂激励环境下分布式结构的振动主动控制研究[D]. 南京：南京航空航天大学, 2012: 105-116.
[34]SHAO M Q.Active vibration control of distributed structures suffering from complex excitations[D]. Nan-jing: Nanjing University of Aeronautics and Astronautics, 2012: 105-116(in Chinese).
[35]姚晓成, 赵程, 曾涛.压电材料在振动控制领域的研究进展与应用现状[J].机械工程材料, 2019, 43(6):72-76
[36]YAO X C, ZHAO C, ZENG T.Research progress and application status of piezoelectric materials for vibration control[J].Materials for mechanical engineering, 2019, 43(6):72-76
[37]WIMMEL R, FEHREN H, GNAUERT U, et al.5 dof active vibration control with a piezoceramic driven multi-functional interface for high load applica-tions[C]//Seventh International Conference on Adaptive Structures, DLR, 1997: 61-70.
[38]鲁继文.风洞模型支杆系统设计及振动主动控制[D]. 大连：大连理工大学, 2018: 6-10.
[39]LU J W.The design of sting system in wind tunnels and active control of vibration[D]. Dalian: Dalian University of Technology, 2018: 6-10(in Chinese).
[40]沈星, 涂凡凡, 陈金金, 等.风洞悬臂杆结构主动减振系统的研究[J].振动、测试与诊断, 2014, 34(3):414-421
[41]SHEN X, TU F F, CHEN J J, et al.Study of active damping system for the cantilever sting in wind tunnel based on piezoelectric actuators[J].Journal of vibration, measurement and diagnosis, 2014, 34(3):414-421
[42]CHEN J J, SHEN X, TU F F, et al.Experimental re-search on an active sting damper in a low speed acoustic wind tunnel[J].shock and Vibration, 2014, 10(7):1-10
[43]BALAKRISHNA S, HOULDEN H, BUTLER D.et al. Development of a wind tunnel active vibration reduc-tion system[C]//45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada: AIAA, 2007: 961-973.
[44]涂凡凡.人工神经网络在压电主动减振系统中的应用研究[D]. 南京：南京航空航天大学, 2013: 38-39.
[45]TU F F.Research on artificial neural network application in active damping system using piezoelectric actuators[D]. Nanjing: Nanjing University of Aeronautics and Astro-nautics, 2013: 38-39(in Chinese).
[46]FEHREN H, GNAUERT U, WIMMEL R, et al.Valida-tion testing with the active damping system in the Euro-pean transonic wind tunnel[C]\\39th Aerospace Sciences Meeting and Exhibit, AIAA, 2001: 0610-0618.
[47]杨智春, 王巍, 谷迎松, 等.一种弯曲型压电堆作动器的设计及在振动控制中的应用[J].振动与冲击, 2009, 28(9):130-136
[48]YANG Z C, WANG W, GU Y S, et al.Smart structure vibration control using a new bending type of pie-zoceramic stack actuator[J].Journal of vibration and shock, 2009, 28(9):130-136
[49]宋来收, 夏品奇.采用压电叠层作动器的弹性梁振动主动控制实验研究[J].[J].航空学报,, 22014, 35(1):171-178
[50]SONG L S, XIA P Q.Experimental investigation on active vibration control of elastic beam by using piezoe-lectric stack actuator[J].Acta aeronautica et astronautica sinica, 2014, 35(1):171-178
[51]刘伟国.支杆式风洞模型主动振动抑制控制方法研究[D]. 大连：大连理工大学, 2015: 43-78.
[52]LIU W G.The study on control methods of the active vibration reduction system of wind tunnel model with sting support[D]. Dalian: Dalian University of Technolo-gy, 2015: 43-78(in Chinese).
[53]姜尔东.支杆式风洞模型主动振动抑制方法与实验研究[D]. 大连：大连理工大学, 2014: 23-54.
[54]JIANG E D.Method and experiment research on the active vibration control of wind tunnel model with sting support[D]. Dalian: Dalian University of Technology, 2014: 23-54(in Chinese).
[55]Balakrishna S, Butler D, Acheson M, et al.Design and performance of an active sting damper for the NASA common research model[C]//49th AIAA Aerospace Sci-ences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida: AIAA, 2011: 953-962.
[56]陈陆军, 车兵辉, 黄勇, 等.低速风洞试验模型振动主动控制技术[J].南京航空航天大学学报, 2021, 53(4):591-597
[57]CHEN L J，CHE B H，HUANG Y，et al.Active vibration control method for test model in low speed wind tunnel[J].Journal of Nanjing University of Aero-nautics & Astronautics, 2021, 53(4):591-597
[58]余立, 杨兴华, 寇西平, 等.跨声速风洞模型主动减振系统试验研究[J].南京航空航天大学学报, 2019, 51(4):526-533
[59]YU L, YANG X H, KOU X P, et al.Experiment on active vibration reduction system for transonic wind tun-nel model[J].Journal of Nanjing University of Aero-nautics & Astronautics, 2019, 51(4):526-533
[60]曾开春, 欧阳炎, 寇西平, 等.风洞模型主动减振结构作动器效率定量表征与提升研究[J].振动与冲击, 2022, 41(18):166-176
[61]ZENG K C, OUYANG Y, KOU X P, et al.Quantifica-tion and improvement of the actuator effectiveness of an active damper for wind tunnel tests[J].Journal of vibra-tion and shock, 2022, 41(18):166-176
[62]曾开春, 寇西平, 杨兴华, 等.跨声速风洞试验模型主动减振结构优化设计[J].航空学报, 2022, 43(2):224944-0
[63]ZENG K C, KOU X P, YANG X H, et al.Optimization of active vibration damping structure for transonic wind tunnel test model[J].Acta aeronautica et astronautica sini-ca, 2022, 43(2):224944-0
[64]梁力, 杨智春, 欧阳炎, 等.垂尾抖振主动控制的压电作动器布局优化[J].航空学报, 2016, 37(10):3035-3043
[65]LIANG L, YANG Z C, OUYANG Y, et al.Optimization of piezoceramic actuator configuration on a vertical tail for buffeting control[J].Acta aeronautica et astronautica sinica, 2016, 37(10):3035-3043
[66]BRUANT I, GALLIMARD L, NIKOUKA S.Optimal piezoelectric actuator and sensor location for active vibration control using genetic algorithm[J],[J].Journal of Sound and Vibration,, 2010,, 329(10):1615-1635
[67]HU K M, LI HUA.Multi-parameter optimization of piezoelectric actuators for multi-mode active vibration control of cylindrical shells[J],[J].Journal of Sound and Vibration,, 2018, 426(10):166-185
[68]麻越垠, 陈万华, 王元兴, 等.风洞模型支撑系统振动主动控制试验研究[J].机械强度, 2015, 37(2):232-236
[69]MA Y Y, CHEN W H, WANG Y X, et al.active vibra-tion control experimental investigation on wind tunnel model support system[J].Journal of mechanical strength, 2015, 37(2):232-236
[70]刘巍, 毕晓丹, 贾振元, 等.风洞模型主动抑制器的设计与实验[J].光学精密工程, 2014, 23(10):2895-2901
[71]LIU W, BI X D, JIA Z Y, et al.design and experiment on active damper of wind tunnel model[J].Optics and preci-sion engineering, 2015, 23(10):2895-2901
[72]DAI Y K, SHEN X, ZHANG L, et al.System identifica-tion and experiment evaluation of a piezoelectric-based sting damper in a transonic wind tunnel[J].Review of scientific instruments, 2019, 90(10):075102-0
[73]姚壮.基于神经网络模型的风洞模型抑振研究[D]. 大连：大连理工大学, 2020: 18-61.
[74]YAO Z.Research on vibration suppression of wind tunnel model based on neural network model[D]. Da-lian: Dalian University of Technology, 2020: 18-61(in Chinese).
[75]张家昆.基于时滞与模糊滑模的风洞模型振动控制研究[D]. 大连：大连理工大学, 2018: 47-66.
[76]ZHANG J K.Research on vibration control of wind tunnel model based on time delay and fuzzy sliding mode[D]. Dalian: Dalian University of Technology, 2018: 47-66(in Chinese).
[77]陈万华, 王元兴, 沈星, 等.压电叠堆主动减振的神经网络实时控制[J].南京航空航天大学学报, 2014, 46(4):587-594
[78]CHEN W H, WANG Y X, SHEN X, et al.Neural net-work PID real-time control for active vibration reduction using piezoceramics stacks[J].Journal of Nanjing Uni-versity of Aeronautics & Astronautics, 2014, 46(4):587-594
[79]DAI Y, ZHANG L, ZHAO Z P, et al.Wind tunnel eval-uation for an active sting damper using multimodal neural networks[J],[J].AIAA Journal, 2020, 58(8):1939-1948
[80]LIU W, LIU W X, ZHOU M D, et al.An active vibration control method based on energy-fuzzy for cantilever structures excited by aerodynamic loads[J],[J].Chinese journal of aeronautics, 2021, 34(9):224-235
[81]HASSANI V, TJAHJOWIDODO T, THANH N D.A survey on hysteresis modeling, identification and con-trol[J],[J].Mechanical Systems and Signal Processing, 2014, 49(5):209-223
[82]李伟光.风洞模型尾撑结构振动压电主动控制研究[D]. 西安：西北工业大学, 2023: 41-64.
[83]LI W G.Research on piezoelectric active vibration con-trol of wind tunnel model tail support structure[D]. Xi' an: Northwestern Polytechnical University, 2023: 41-64(in Chinese).
[84]胡寿松, 王执铨, 胡维礼.最优控制理论与系统(第2版)[M] 北京：科学出版社. 2005:
[85]HU S S, WANG Z Q, HU W L.Optimal Control Theory and Systems(2nd edition)[M]. Beijing: Science press(in Chinese).Beijing: Science press, 2005, 0(0):2-7
[86]张家昆, 贾振元, 刘昱, 等.基于时滞算法的风洞模型振动控制试验研究[J].新技术新工艺, 2018, 9(9):32-37
[87]ZHANG J K, JIA Z Y, LIU Y, et al.Research on experi-ment of vibration control of wind tunnel model based on time-delay LQR algorithm[J].[J].New technology and new process., 2018, 9(9):32-37
[88]佘重禧, 陈卫东, 邵敏强.跨声速风洞测力模型的降阶及∞减振控制[J].噪声与振动控制, 2014, 34(1):67-72
[89]SHE C X, CHEN W D, SHAO M Q.Model reduction and active vibration suppression of a wind tunnel test model by H∞ control[J].Noise and vibration control, 2014, 34(1):67-72
[90]佘重禧.跨声速风洞测力试验模型的振动主动控制研究[D]. 南京：南京航空航天大学, 2013: 45-58.
[91]SHE C X.Study on active vibration control for wind tunnel testing model in transonic test[D]. Nanjing: Nan-jing University of Aeronautics and Astronautics, 2013: 45-58(in Chinese).
[92]汪建晓, 孟光.磁流变液研究进展[J].航空学报, 2001, 23(1):6-12
[93]WANG J X, MENG G.Research advances in magne-torheological fluids[J].Acta aeronautica et astronautica sinica, 2001, 23(1):6-12
[94]卢坤, 刘翎, 杨志荣, 等.基于磁流变弹性体的推进轴系半主动式吸振器研究[J].振动与冲击, 2017, 36(15):36-42
[95]LU K, LIU L, YANG Z R, et al.Semi-active dynamic absorber of a ship propulsion shafting based on MREs[J].Journal of vibration and shock, 2017, 36(15):36-42
[96]汪路路.1.2米风洞磁流变减振系统研制报告[R]. 绵阳: 中国空气动力研究与发展中心, 2023.
[97]WANG L L.Vibration damping system based on magne-torheological fluids in 1.2 meter scale wind tunnel[R]. Mianyang: China aerodynamics research and develop-ment center, 2023.
[98]杨铁军, 石慧, 李新辉, 等.一种基于智能减振器的船舶机械设备主动减振系统研制[J].振动工程学报, 2017, 30(2):167-176
[99]YANG T J, SHI H, LI X H, et al.One active isolation system for marine machine based on smart isolators[J].Journal of vibration engineering, 2017, 30(2):167-176
[100]廖达雄, 黄之龙, 陈振华, 等.大型低温高雷诺数风洞及其关键技术综述[J].实验流体力学, 2014, 28(2):1-7
[101]LIAO D X, HUANG Z L, CHEN Z H, et al.Review on large-scale cryogenic wind tunnel and key technology[J].Journal of experiments in fluid mechanics, 2014, 28(2):1-7
[102]王长军.低温工程用 18Ni200D 锻件技术条件[R]. 北京: 钢铁研究总院有限公司, 2022.
[103]WANG C J.Technical specifications of 18Ni200D steel forgings in cryogenic engineering[R]. Beijing: Central iron and steel research institute, 2002.
[104]PHILIP S A, DANA J J, MICHAEL B, et al.Wind tunnel and propulsion test facilities supporting analyses to an assessment of NASA' s capabilities to serve national needs[R]. Arlington, VA: RAND National defense re-search institute, 2004.
[105]Acheson M, Balakrishna S.Effects of active sting damp-ing on common research model data quality[C]//49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida: AIAA, 2011: 878-901.
[106]杨兴华.某低温风洞模型减振系统结构设计与保温方案验证报告[R]. 绵阳: 中国空气动力研究与发展中心, 2021.
[107]YANG X H.Verification report on structure design and insulation scheme of cryogenic wind tunnel model vibra-tion reduction system[R]. Mianyang: China aerodynam-ics research and development center, 2021.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

风洞试验模型振动机理及主动控制研究进展

A Review of Model Vibration Mechanism and Active Control in Wind Tunnel Test

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	孙朋朋, 刘平安, 樊枫, 曾伟. 悬停状态共轴刚性旋翼机身气动干扰特性[J]. 航空学报, 2024, 45(9): 529284-529284.
[2]	王畅, 何龙, 徐栋霞, 唐敏, 马率, 吴希明. 共轴刚性旋翼桨毂流动控制减阻研究[J]. 航空学报, 2024, 45(9): 529084-529084.
[3]	张卫国, 唐敏, 武杰, 彭先敏, 章贵川, 聂博文, 王亮权, 李超群. 倾转旋翼机风洞试验综述[J]. 航空学报, 2024, 45(9): 530114-530114.
[4]	聂博文, 王亮权, 黄志银, 何龙, 杨仕鹏, 颜鸿涛, 章贵川. 复合式高速无人直升机飞行动力学建模与控制策略设计[J]. 航空学报, 2024, 45(9): 529848-529848.
[5]	刘柳, 向先宏, 张宇飞, 陈海昕, 魏闯, 朱剑, 杨普. 一种高升阻比非常规翼身融合燕尾气动布局[J]. 航空学报, 2024, 45(6): 629630-629630.
[6]	李海星, 周峰, 颜巍, 白峰, 赵克良. 砂纸冰对民机平尾气动特性的影响[J]. 航空学报, 2024, 45(2): 128657-128657.
[7]	李学良, 李创创, 苏伟, 吴杰. 分布式粗糙元对高超声速边界层不稳定性的影响试验[J]. 航空学报, 2024, 45(2): 128627-128627.
[8]	刘宇, 秦梦婕, 王强, 易贤. 含盐海水飞沫的结冰风洞试验相似准则[J]. 航空学报, 2023, 44(S2): 729297-729297.
[9]	杨秋明, 朱永峰, 陈华伟, 刘晓林. 镂空图案化电加热组件防冰性能试验研究[J]. 航空学报, 2023, 44(S2): 729334-729334.
[10]	高世琦, 丁博, 解旭祯, 李铮, 陈林, 钱首元, 焦子涵, 白光辉. 等离子体激励在高速流动中的减阻机制[J]. 航空学报, 2023, 44(S2): 729373-729373.
[11]	许岭松, 吴渊, 朱东宇, 张付昆, 刘昱. FL⁃61结冰风洞翼型俯仰振荡机构研制[J]. 航空学报, 2023, 44(S2): 729296-729296.
[12]	金毅, 孙姝, 郭赟杰, 谭慧俊, 张悦. 超声速可调进气道内流双解现象及其节流特性[J]. 航空学报, 2023, 44(7): 127134-127134.
[13]	李俊红, 靳旭红, 刘春风, 苗文博, 程晓丽. 临近空间高速飞行器微量气动力试验及计算[J]. 航空学报, 2023, 44(6): 127072-127072.
[14]	曾宪昂, 赵冬强, 李俊杰, 严泽洲, 刘成玉. 弹性机翼阵风减缓控制策略风洞试验[J]. 航空学报, 2023, 44(4): 226869-226869.
[15]	刘畅, 张耘隆, 闫指江, 赵磊, 季辰. 锤头体火箭弹性模型脉动压力风洞试验[J]. 航空学报, 2023, 44(23): 128384-128384.