Review on buzz wind tunnel test technology for aircraft control surfaces

YAN Yu; LU Bo; YANG Xinghua; GUO Hongtao; YU Li

doi:10.7638/kqdlxxb-2021.0303

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Review on buzz wind tunnel test technology for aircraft control surfaces

更新时间：2026-05-28

- Review on buzz wind tunnel test technology for aircraft control surfaces
- Vol. 40, Issue 3, Pages: 1-9(2022)
- 作者机构：
  
  中国空气动力研究与发展中心高速空气动力研究所,绵阳,621000
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2021.0303
  CLC： V211.71;V216.2+4
- Published：2022
- 稿件说明：
移动端阅览
闫昱, 路波, 杨兴华, 等. 飞行器操纵面嗡鸣风洞试验技术综述[J]. 空气动力学学报, 2022, 40(3): 1−9.

YAN Yu, LU Bo, YANG Xinghua, et al. Review on buzz wind tunnel test technology for aircraft control surfaces[J]. 2022, 40(3): 1-9.
闫昱, 路波, 杨兴华, 等. 飞行器操纵面嗡鸣风洞试验技术综述[J]. 空气动力学学报, 2022, 40(3): 1−9. DOI： 10.7638/kqdlxxb-2021.0303

YAN Yu, LU Bo, YANG Xinghua, et al. Review on buzz wind tunnel test technology for aircraft control surfaces[J]. 2022, 40(3): 1-9. DOI： 10.7638/kqdlxxb-2021.0303.

摘要

操纵面嗡鸣是飞行器跨声速飞行时发生的气动弹性动不稳定现象。嗡鸣的发生，轻则降低飞行器操纵面效率，重则导致灾难性的飞行事故，是除颤振外飞行器设计部门重点关注的气动弹性难题。操纵面嗡鸣涉及激波与边界层的相互作用，目前尚没有准确预测嗡鸣的计算方法，通常采用风洞试验来获取相关数据。操纵面嗡鸣风洞试验可以利用风洞再现嗡鸣现象，研究嗡鸣特性，是飞行器研制阶段检验操纵面防嗡鸣设计最行之有效的手段。本文回顾了国内外操纵面嗡鸣风洞试验研究现状，梳理了操纵面嗡鸣的发生机理、触发条件及分型依据，对操纵面嗡鸣试验风洞选取、模型设计、试验方法提供了建议，对颤振试验中可能出现的嗡鸣问题提供了判别方法，对后续的工作进行了展望。

Abstract

Control surface buzz of the aircraft is an aeroelastic instability phenomenon during the transonic flight. The occurrence of buzz can reduce the efficiency of aircraft control surfaces

and even cause disastrous flight accidents. Therefore

the buzz phenomenon is another difficult aeroelastic problem that the aircraft design department focuses on in addition to the flutter. Control surface buzz is related to the interaction between the shock wave and the boundary layer

and there is no accurate calculation method to obtain the buzz characteristics

thus the wind tunnel test is usually used to acquire relevant data. The buzz wind tunnel test can be used to reproduce the buzz phenomenon and study its characteristics

which is the most effective method to verify the anti-buzz design in the aircraft development stage. In the present study

we review previous studies of buzz wind tunnel tests. The occurrence mechanism

triggering conditions and control surface buzz classification are sorted out. Feasible suggestions for suitable wind tunnel selection

model design and test methods of buzz wind tunnel test are provided

and effective methods to distinguish the buzz phenomenon during the flutter test are discussed. The follow-up work is presented in the end.

关键词

Keywords

references

ZHANG W W, GAO C Q, YE Z Y. The complex transonic aeroelastic phenomena and it's mechanisms[J]. Chinese Science Bulletin, 2018, 63(12): 1095-1110. (in Chinese)

王发祥. 高速风洞试验[M]. 北京: 国防工业出版社, 2003: 437.

STEGER J L, BAILEY H E. Calculation of transonic aileron buzz[J]. AIAA Journal, 1980, 18(3): 249-255. DOI:10.2514/3.50756

BENDIKSEN O. Nonclassical aileron buzz in transonic flow[C]//34th AIAA, ASME, ASCE, AHS, and ASC, Structures, Structural Dynamics and Materials Conference. AIAA and ASME, Adaptive Structures Forum. La Jolla, CA, 1993: 19-22. AIAA-93-1479. doi: 10.2514/6.1993-1479

FUGLSANG D, BRASE L, AGRAWAL S. A numerical study of control surface buzz using computational fluid dynamic methods[C]//10th Applied Aerodynamics Conference, Palo Alto, CA, USA. Reston, Virigina: AIAA, 1992. AIAA-92-2654. doi: 10.2514/6.1992-2654

HUTTSELL L, SCHUSTER D, VOLK J, et al. Evaluation of computational aeroelasticity codes for loads and flutter[C]//39th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 2001. AIAA-01-0569. doi: 10.2514/6.2001-569

SHI A M, YANG Y N, YE Z Y. Investigation of control surface buzz in transonic flow[J]. Journal of Northwestern Polytechnical University, 2004, 22(4): 525-528. (in Chinese)

ANDERSON W, MORTARA S. F-22 aeroelastic design and test validation[C]//48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii. Reston, Virigina: AIAA, 2007. AIAA 2007-1764. doi: 10.2514/6.2007-1764

邓俊艳, 周伟, 易军, 等. 操纵面嗡鸣工程判别及预防[C]//第十六届全国空气弹性学术交流会会议, 2019: 624-625.

杨超, 主编. 飞行器气动弹性原理[M]. 北京: 北京航空航天大学出版社, 2011: 123.

李周复, 主编. 风洞特种试验技术[M]. 北京: 航空工业出版社, 2010: 201-207.

ERICKSON A L, STEPHENSON J D. A suggested me-thod of analyzing for transonic flutter of control surfaces based on available experimental evidence [R ] . NACA-RM-A7F30, 1947. https://ntrs.nasa.gov/api/citations/19930085716/downloads/19930085716.pdf

PARKER E, SPAIN C, SOISTMANN D. Aileron buzz investigated on several generic NASP wing configurations[C]//32nd Structures, Structural Dynamics, and Materials Conference, Baltimore, MD, USA. Reston, Virigina: AIAA, 1991. AIAA-91-0936-CP. doi: 10.2514/6.1991-936

SAITON K, TAMAYAMA M, KIKUCHI T, et al. An aileron flutter experiment and analysis using Semi-Span model for the small supersonic experimental aircraft[C ] //Japan Society of Aeronautical Space Sciences, 2012, 60: 108-113. https://www.jstage.jst.go.jp/article/jjsass/60/2/60_2_108/_pdf/-char/en doi: 10.2322/jjsass.60.108

PHILLIPS W H, ADAMS J J. Low-speed tests of a model simulating the phenomenon of control-surface buzz[R ] . NACA-RM-L50F19, 1950. https://ntrs.nasa.gov/api/citations/19930087842/downloads/19930087842.pdf

HENNING A B. Results of a rocket-model investiga-tion of control-surface buzz and flutter on a 4-percent-thick unswept wing and on 6-, 9-, and 12-percent-thick swept wings at transonic speeds[C ] . NACA-RM-L53I29, 1953. https://ntrs.nasa.gov/api/citations/19930089146/downloads/19930089146.pdf

LAMBOURNE N C. Control-surface buzz[R ] . ARC/RM-3364, 1963. https://naca.central.cranfield.ac.uk/bitstream/handle/1826.2/3947/arc-rm-3364.pdf?sequence = 1isAllowed = y

NAKAMURA Y. Some contributions on a control-surface buzz at high subsonic speeds[J]. Journal of Aircraft, 1968, 5(2): 118-125. DOI:10.2514/3.43918

DAI J, LIU Q G. Calculation of transonic control surface buzz[J]. Acta Aerodynamica Sinica, 1997, 15(3): 366-371. (in Chinese)

LIU Q G, DAI J, BAI J Q. Hopf bifurcation analysis of transonic control surface buzz and investigation of the influence of structural parameters on buzz characteristics[J]. Acta Aeronautica et Astronautica Sinica, 1999, 20(6): 527-532. (in Chinese)

YANG G W, OBAYASHI S, NAKAMICHI J. Aileron buzz simulation using an implicit multiblock aeroelastic solver[J]. Journal of Aircraft, 2003, 40(3): 580-589. DOI:10.2514/2.3134

SHI A M, YANG Y N, YE Z Y. Relatively accurate calculation of 3-D control surface buzz in transonic flow[J]. Journal of Northwestern Polytechnical University, 2006, 24(5): 537-540 (in Chinese).

ZHANG W W, YE Z Y, SHI A M, et al. Numerical analysis for B-type buzz and C-type buzz basing on Euler codes[J]. Journal of Vibration Engineering, 2005, 18(4): 458-464. (in Chinese)

XU J, MA X P. Buzz aeroelastic responses analysis for a flying wing UAV[J]. Journal of Northwestern Polytechnical University, 2015, 33(4): 588-595. (in Chinese)

XU J, MA X P. Transonic rudder buzz investigated on a tailless flying wing UAV[J]. Transactions of Nanjing University of Aeronautics Astronautics, 2015, 32(1): 61-69.

XU J, MA X P. Research on flying wing UAV buzz vibration considering the aerodynamic structural coupling effects[J]. Journal of Air Force Engineering University (Natural Science Edition), 2016, 17(3): 6-10. (in Chinese)

HE S. Study on wing nonlinear flutter in transonic flow[D]. Xi'an: Northwestern Polytechnical University, 2017: 27-49 (in Chinese).

HE S, YANG Z C, GU Y S. Limit cycle oscillation behavior of transonic control surface buzz considering free-play nonlinearity[J]. Journal of Fluids and Structures, 2016, 61: 431-449. DOI:10.1016/j.jfluidstructs.2015.11.014

GAO C Q, ZHANG W W, YE Z Y. A new viewpoint on the mechanism of transonic single-degree-of-freedom flutter[J]. Aerospace Science and Technology, 2016, 52: 144-156. DOI:10.1016/j.ast.2016.02.029

GAO C Q, ZHANG W W. Study on the mechansim and instability parameters of transonic buzz[J]. Acta Aerodynamica Sinica, 2019, 37(1): 99-106. (in Chinese)

申超峰. 某飞机方向舵振动试验报告[R]. 绵阳: 中国空气动力研究与发展中心, 1974.

陈忠实. 某飞机方向舵嗡鸣试验报告[R]. 绵阳: 中国空气动力研究与发展中心, 1977.

KOU X P. Research on high speed static aeroelastic model design of high-aspect-ratio wing[D]. Mianyang: CARDC, 2013: 44 (in Chinese).

LUO W K, TAN S G, XIE H Q, et al. Research on methods used to determine flutter model design factors[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(10): 2383-2390. (in Chinese)

QIAN W, ZHANG G J, LIU Z K. Flutter characteristics for aircraft all-movable horizontal tail through wind tunnel test[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(4): 1093-1102. (in Chinese)

SUN Y J, LIANG J, YANG F, et al. Transonic flutter wind tunnel tests for an aircraft with a supercritical wing[J]. Journal of Vibration and Shock, 2014, 33(4): 190-194. (in Chinese)

RAN Y G, LI Q Y, YANG X H. Review of transonic flutter test techniques for statically unstable aircraft scaled model[J]. Journal of Sichuan University of Science Engineering (Natural Science Edition), 2017, 30(1): 49-54. (in Chinese)

RIVERA J A, FLORANCE J R. Contributions of transonic dynamic tunnel testing to airplane flutter clearance[R ] . AIAA 2000-1768, 2000. https://ntrs.nasa.gov/api/citations/20000037720/downloads/20000037720.pdf

杨祖清, 主编. 流动显示技术[M]. 北京: 国防工业出版社, 2002: 101-131.

GAO L M, WU Y N, HU X Q, et al. Intensity-based fast response PSP technique and its applications[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3): 607-623. (in Chinese)

MERIENNE M C, LE SANT Y, LEBRUN F, et al. Transonic buffeting investigation using unsteady pressure-sensitive paint in a large wind tunnel[C]//51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine (Dallas/Ft. Worth Region), Texas. Reston, Virginia: AIAA, 2013. doi: 10.2514/6.2013-1136

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