高超声速飞行器气动弹性力学研究综述

流体力学、飞行力学与发动机

本期目录 | 过刊浏览 | 高级检索

| 后一篇

高超声速飞行器气动弹性力学研究综述

杨超，许赟，谢长川

北京航空航天大学航空科学与工程学院

收稿日期:2008-11-18 修回日期:2009-01-09 出版日期:2010-01-25 发布日期:2010-01-25
通讯作者: 杨超

Review of Studies on Aeroelasticity of Hypersonic Vehicles

Yang Chao, Xu Yun, Xie Changchuan

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics

Received:2008-11-18 Revised:2009-01-09 Online:2010-01-25 Published:2010-01-25
Contact: Yang Chao

摘要/Abstract

摘要： 高超声速飞行器设计上的特点带来了一系列的气动弹性新问题。本文回顾高超声速飞行器气动弹性研究的历史与现状，着重介绍和分析了高超声速非定常气动力计算方法、热环境下的气动弹性问题、壁板颤振、推力影响下的气动弹性稳定性问题以及气动推进/气动弹性耦合的多学科交叉问题，相关的主动控制方法的研究进展亦有所介绍。在已有气动弹性问题研究发展的基础上，提出了高超声速飞行器在气动弹性领域需要解决和关注的若干问题，包括高超声速气动弹性试验、燃料消耗的质量变化对于飞行器气动弹性特性的影响以及气动弹性力学与飞行力学综合等方面。

关键词: 气动弹性, 颤振, 高超声速气动力, 气动加热, 振动, 飞行器推进系统, 高超声速

Abstract: There are many new problems of aeroelasticity which are introduced by the novel concepts and system characteristics in the design process of hypersonic vehicles. An overview of the studies on aeroelasticity of hypersonic vehicles is presented here. Special attention is paid to the following areas: the compute method of unsteady aerodynamics in hypersonic flow; aeroelastic characteristics with temperature effects; panel flutter in hypersonic flow; thrust induced instability of aeroelasticity; the coupling problem of aerodynamics, propulsion and aeroelasticity; and also the active control methods used in the solutions of these problems. Finally, based on the progress of existing research in these areas, some key issues are introduced which deserve more attention of the researchers’ for solution. These include: experimental research on hypersonic aeroelasticity, effect of mass variety on the characteristics of aeroelasticity which is caused by the consumption of the fuels, and integration analysis of aeroelasticity and flight dynamics.

Key words: aeroelasticity, flutter, hypersonic aerodynamic, aerodynamic heating, vibration, aircraft propulsion, hypersonic

中图分类号:

V215.3

杨超;许赟;谢长川. 高超声速飞行器气动弹性力学研究综述[J]. 航空学报, 2010, 31(1): 1-11.

Yang Chao;Xu Yun;Xie Changchuan. Review of Studies on Aeroelasticity of Hypersonic Vehicles[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 1-11.

参考文献

［1］Dana W. The X-15 airplane -lessons learned［R］.AIAA-1993-0309, 1993. ［2］Chase R L, Tang M H. A history of the NASP program from the formation of the joint program office to the termination of the HySTP scramjet performance demonstration program［R］. AIAA-1995-6031, 1995. ［3］Peebles C. The X-43A flight research program: lessons learned on the road to Mach 10［M］. Washington, D. C.: AIAA Inc., 2007. ［4］Walker S, Rodgers F. Falcon hypersonic technology overview［R］. AIAA-2005-3253, 2005. ［5］Spain C, Soistmann D, Parker E, et al. An overview of selected NASP aeroelastic studies at the NASA langley research center［R］. AIAA-1990-5218, 1990. ［6］Michael W K, Todd S. Thermoelastic test techniques［R］. NASA TM-101747, 1991. ［7］Rodgers J P. Aerothermoelastic analysis of a NASP-like vertical fin［R］. AIAA-1992-2400, 1992. ［8］Spain Charles V, Zeiler T A, Bullock Ellen P, et al. A flutter investigation of all-moveable NASP-like wings at hypersonic speeds［R］. AIAA-1993-1315, 1993. ［9］Cole S R, Florance J R, Thomason L B, et al. Supersonic aeroelastic instability results for a nasp-like wing model［R］. AIAA-1993-1369, 1993. ［10］Heeg J, Zeiler T, Pototzky A, et al. Aerothermoelastic analysis of a NASP demonstrator model［R］. AIAA-1993-1366, 1993. ［11］Pak C G, Baker M L. Control surface buzz analysis of a generic NASP wing［R］. AIAA-2001-1581, 2001. ［12］Lawrence J O. Aerothermoelasticity: its impact on stability and control of wingedaerospace vehicles［J］. Journal of Aircraft, 1965, 2(6):517-526. ［13］Ericsson E L. Hypersonic aerothermoelastic characteristics of a finned missile［J］. Journal of Spacecraft, 1979, 16(3):187-190. ［14］Friedmann P P. Hypersonic aeroelasticity and aerothermoelasticity with application to reusable launch vehicles［R］. AIAA-2003-7014, 2003. ［15］Heeg J, Gilbert M G, Pototzky A S. Active control of aerothermoelastic effects for a conceptual hypersonic aircraft［J］. Journal of Aircraft, 1993, 30(4): 453-458. ［16］惠俊鹏. 热环境下翼面颤振分析与颤振主动抑制研究［D］. 北京：北京航空航天大学，2006. Hui Junpeng. Hypersonic flutter analysis for wings undue thermal circumstances and active flutter suppression［D］. Beijing: Beijing University of Aeronautics and Astronautics, 2006. (in Chinese) ［17］Wu Z G, Yang C. Flight loads and dynamics of flexible air vehicles［J］. Chinese Journal of Aeronautics, 2004, 17(1): 17-22. ［18］Lees L. Hypersonic flow［C］∥Proceedings of the Fifth International Aeronautic Conference. 1955. ［19］Lighthill M J. Oscillating airfoils at high mach numbers［J］. Journal of the Aeronautical Sciences, 1953, 20(6):402-406. ［20］Ashley H, Zartarian G. Piston theory—a new aerodynamic tool for the aeroelastician［J］. Journal of the Aeronautical Sciences, 1956, 23(12): 1109-1118. ［21］陈劲松, 曹军. 超声速和高超声速翼型非定常气动力的一种近似计算方法［J］. 空气动力学学报, 1990, 8(3): 339-344. Chen Jinsong, Cao Jun. An approximate calculating method of supersonic/hypersonic unsteady aerodynamic forces of airfoils［J］. Acta Aerodynamica Sinica, 1990, 8(3): 339-344. （in Chinese） ［22］杨炳渊，宋伟力. 用当地流活塞理论计算大攻角翼面超声速颤振［J］. 振动与冲击, 1995, 15(2): 60-63. Yang Bingyuan, Song Weili. Supersonic flutter calculation of a wing with attack angle by local flow piston theory［J］. Journal of Vibration And Shock, 1995, 15(2): 60-63. （in Chinese） ［23］张伟伟, 叶正寅. 基于当地流活塞理论的气动弹性计算方法研究［J］. 力学学报, 2005, 37(5): 632-639.  Zhang Weiwei, Ye Zhengyin. Numerical method of aeroelasticity based on local Piston theory［J］. Acta Mechanica Sinica, 2005, 37(5): 632-639. （in Chinese） ［24］Yao Z X, Liu D D. From piston theory to unified hypersonic-supersonic lifting surface method［J］. Journal of Aircraft, 1997, 34(3): 304-312. ［25］Zaero theoretical manual (Version 7.3)［CP］. Scottsale, A. Z., USA: ZONA Technology, Inc., 2005. ［26］Hui W H. Unified unsteady supersonic/hypersonic theory of flow past double wedge airfoils［J］. Journal of Applied Mathematics and Physics, 1983, 34(4): 458-488. ［27］Liu D D, Chen P C, Tang L, et al. Expedient hypersonic aerothermodynamics methodology for RLV/TPS design［R］. AIAA-2002-5129, 2002. ［28］Thuruthimattam B J, Friedmann P P, Powell K G, et al. Aeroelasticity of a generic hypersonic vehicle［R］. AIAA-2002-1209, 2002. ［29］Thuruthimattam B J, Friedmann P P, Mcnamara J J, et al. Modeling approaches to hypersonic aeroelasticity［C］∥ASME International Mechanical Engineering Congress and Exposition. New Orleans, Louisiana, USA: ASME, 2002. ［30］Thuruthimattam B J, Friedmann P P, Mcnamara J J, et al. Modeling approaches to hypersonic aerothermoelasticity with application to reusable launch vehicles［R］. AIAA-2003-1967, 2003. ［31］Mcnamara J J, Thuruthimattam B J, Friedmann P P, et al. Hypersonic aerothermoelastic studies for reusable launch vehicles［R］. AIAA-2004-1590, 2004. ［32］Bartels R E, Rumsey C L, Biedron R T. CFL3D version 6.4—general usage and aeroelastic analysis［R］. NASA TM-2006-214301, 2006. ［33］McNamara J J, Friedmann P P, Powell K G, et al. Three-dimensional aeroelastic and aerothermoelastic behavior in hypersonic flow［R］. AIAA-2005-2175, 2005. ［34］Roger M. Aerothermoelasticity［J］. Aerospace Engineering, 1958(2):162-166. ［35］吴志刚, 惠俊鹏, 杨超. 高超声速下翼面的热颤振工程分析［J］. 北京航空航天大学学报, 2005,31(3): 270-273. Wu Zhigang, Hui Junpeng, Yang Chao. Hypersonic aerothermoelastic analysis of wings［J］. Journal of Beijing University of Aeronautics and Astronautics,2005,31(3): 270-273. (in Chinese) ［36］Ericsson L E, Almroth B O, Bailie J A. Hypersonic aerothermoelastic characteristics of a finned missile［J］. Journal of Aircraft, 1979, 16(3): 187-192. ［37］Ricketts R H, Doggett R V, Jr. NASP aeroservothermoelasticity studies［R］. NASA TM-104058, 1991. ［38］Lind R. Linear parameter-varying modeling and control of structural dynamics with aerothermoelastic effects［R］. AIAA-1999-1393, 1999. ［39］Lind R, Buffington J, Sparks A K. Multi-loop aeroservoelastic control of a hypersonic vehicle［R］. AIAA-1999-4123, 1999. ［40］Loehner R, Yang C, Cerbal J, et al. Fluid-structure-thermal interaction using a loose coupling algorithm and adaptive unstructured grids［R］. AIAA-1998-2419, 1998. ［41］McNamara J J. Aeroelastic and aerothermoelastic behavior of two and three dimensional lifting surfaces in hypersonic flow［D］. Ann Arbor, M. I., USA: University of Michigan, 2005. ［42］Lemley C E. Design criteria for prediction and prevention of panel flutter, Vol. I: criteria presentation VII: background and review of state of the art［R］. AFB, O. H., USA: Air Force Flight Dynamic Lab., TR-67-140, 1967. ［43］孟凡颢, 钟腾育. 用壁板颤振理论解决某系列飞机的方向舵蒙皮裂纹故障［J］. 飞机设计, 2000(4): 1-6. Meng Fanhao, Zhong Tengyu. Using panel flutter theory in the solution of skin crackle of rudders［J］. Aircraft Design, 2000(4):1-6. （in Chinese） ［44］Miles J W. Dynamic chordwise stability at supersonic speeds［R］. North American Aviation Report, AL-1140, 1950. ［45］Jordan P. The physical nature of panel flutter［J］. Aero Digest, 1956, 72(2): 34-38. ［46］Bisplinghoff R L. Aeroelasticity［M］. Cambridge, Mass: Addison-Wesley Publishing Company, 1955. ［47］Bisplinghoff R L. Principles of aeroelasticity［M］. New York: John Wiley &Sons, Inc., 1962. ［48］Dowell E H. Aeroelasticity of plates and shells［M］. Leyden: Noordhoff International Pub., 1974. ［49］Xue D Y, Mei C, Shore C P. Finite element two-dimensional panel flutter at high supersonic speeds and elevated temperature［R］. AIAA-1990-982, 1990. ［50］Gray C E, Mei C. Large-amplitude finite element flutter analysis of composite panels in hypersonic flow［J］. AIAA Journal, 1993, 31(6): 1090-1099. ［51］Abbas J F, Ibrahim R A, Gibson R F. Nonlinear flutter of orthotropic composite panel under aerodynamic heating［J］. AIAA Journal, 1993, 31(8): 1478-1488. ［52］Singha M K, Ganapathi M. A parametric study on supersonic flutter behavior of laminated composite skew flat panels［J］. Composite Structures, 2005, 69(1): 55-63. ［53］Xue D Y. A finite element frequency domain solution of nonlinear panel flutter with temperature effects and fatigue life analysis［D］. Norfolk, V. A., USA: Old Donminion University, 1991. ［54］Dhainaut J M. Nonlinear response and fatigue estimation of surface panels to white and non-white gaussian random excitations［D］. Norfolk, V. A., USA: Old Donminion University, 2001. ［55］Scott R C, Weisshaar T A. Panel flutter suppression using adaptive material actuators［J］. Journal of Aircraft, 1994, 31(1): 213-222. ［56］Mei C, Abdel-Motagaly K, Chen R. Review of nonlinear panel flutter at supersonic and hypersonic speeds［J］. Applied Mechanics Reviews, 1999, 52(10): 312-321. ［57］Cheng G F, Mei C. Finite element modal formulation for hypersonic panel flutter analysis with thermal effects［J］. AIAA Journal, 2004, 42(4): 687-695. ［58］杨智春, 夏巍, 孙浩. 高速飞行器壁板颤振的分析模型和分析方法［J］. 应用力学学报, 2006, 23(4): 537-542. Yang Zhichun, Xia Wei, Sun Hao. Analysis of panel flutter in high speed flight vehicles［J］. Chinese Journal of Applied Mechanics, 2006, 23(4):537-542. （in Chinese） ［59］Bolotin V V. Nonconservative problem of the theory of elastic stability［M］. Oxford, UK: Pergamon Press, 1963. ［60］Beal T R. Dynamic stability of a flexible missile under constant and pulsating thrust［J］. Journal of Aircraft, 1965, 3(3): 486-494. ［61］Wu J J. Missile stability using finite elements: an unconstrained variational approach［J］. AIAA Journal, 1976, 14(3): 313-319. ［62］宋健. 在推力和阻力作用下飞行器横向振动分析［J］. 中国工程科学, 2000, 2(10): 66-72. Song Jian. Lateral vibration analyses of flying vehicle under thrust and drag［J］. Engineering Science, 2000, 2(10):66-72. （in Chinese） ［63］Seyranian O N. Optimization of stability of a flexible missile under follower thrust［R］. AIAA-1998-4969,1998. ［64］Pastilha P A. Structural optimization and analysis for flutter instability problems［C］∥International Conference on Engineering Dynamics(ICED). 2007. ［65］Livshits D S, Yaniv S, Karpel M. Dynamic stability of free flight rockets［R］. AIAA-1996-1344, 1996. ［66］Ohshima T, Sugiyama Y. Effect of aerodynamic loads on dynamic stability of slender launch vehicle subjected to an end rocket thrust［C］∥2002 ASME International Mechanical Engineering Congress and Exposition. 2002. ［67］Xu Y, Xie C C, Yang C. Effect of thrust on aeroelastic stability of a slender missile［R］. AIAA-2008-2022, 2008. ［68］Pourtakdoust S H, Assadian N. Investigation of thrust effect on the vibrational characteristics of flexible guided missiles［J］. Journal of Sound and Vibration, 2004, 272(1-2): 287-299. ［69］王其政. 结构耦合动力学［M］. 北京: 中国宇航出版社, 1999. Wang Qizheng. Structural coupling dynamics［M］. Beijing: China Astronautics Publishing House, 1999.（in Chinese） ［70］Fidan B, Mirmirani M, Ioannou P. Flight dynamics and control of air-breathing hypersonic vehicles: review and new directions［R］. AIAA-2003-7081, 2003. ［71］Schmidt D. Dynamics and control of hypersonic aeropropulsive/aeroelastic vehicles［R］. AIAA-1992-4326, 1992. ［72］Chavez F R, Schmidt D K. Analytical aeropropulsive/aeroelastic hypersonic-vehicle model with dynamic analysis［J］. Journal of Guidance, Control, and Dynamics, 1994, 17(6): 1308-1319. ［73］Walton J A. Performance sensitivity of hypersonic vehicles to changes in angle of attack and dynamic pressure［R］. AIAA-1989-2463, 1989. ［74］Raney D L, Mcminn J D, Pototzky A S, et al. Impact of aeroelasticity on propulsion and longitudinal flight dynamics of an air-breathing hypersonic vehicle［R］. AIAA-1993-1367, 1993. ［75］Velapoldi D K. Flight dynamics and feedback guidance issues for hypersonic airbreathing vehicles［R］. AIAA-1999-4122, 1999. ［76］Bolender M A, Doman D B. A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle［R］. AIAA-2005-6255, 2005. ［77］Oppenheimer M, Doman D B. A hypersonic vehicle model developed with piston theory［R］. AIAA-2006-6637, 2006. ［78］Michael A, Doman D B. Nonlinear longitudinal dynamical model of an air-breathig hypersonic vehicle［J］. Journal of Spacecraft and Rockets, 2007, 44(2): 374-387. ［79］Oppenheimer M, Skujins T, Bolender M, et al. A flexible hypersonic vehicle model developed with piston theory［R］. AIAA-2007-6396, 2007. ［80］Schmidt D K. Integrated control of hypersonic vehicles—a necessity not just a possibility［R］. AIAA-1993-3761, 1993. ［81］Buschek H A. Robust control of hypersonic vehicles considering propulsive and aeroelastic effects［R］. AIAA-1993-3726, 1993. ［82］Schmidt F R. Uncertainty modeling for large flexible high-speed aircraft［R］. AIAA-1996-3920, 1996.

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

[1]	孟繁敏, 马诺, 马文朝, 孟军辉, 李文光. 斜掠气梁充气翼湿模态分析与试验[J]. 航空学报, 2023, 44(2): 227098-227098.
[2]	郑锋, 黄薇, 季宏丽, 裘进浩. 复合材料薄板结构中的声学黑洞效应探究[J]. 航空学报, 2023, 44(1): 426453-426453.
[3]	孙志坤, 史志伟, 张伟麟, 李铮, 孙琪杰. 等离子体激励器对高速翼型升阻特性的影响[J]. 航空学报, 2022, 43(S2): 23-39.
[4]	化为卓, 高岭, 陈戈, 李益文, 巩耕, 王延涛, 魏彪. 基于等离子体炬的磁流体动力学实验系统[J]. 航空学报, 2022, 43(S2): 1-7.
[5]	黄依峰, 曾舒华, 江中正, 陈伟芳. 非线性耦合本构在高空侧向喷流中的数值研究[J]. 航空学报, 2022, 43(S2): 8-22.
[6]	罗凯, 王永海, 汪球, 栗继伟, 李峥, 聂春生, 李铮. 高焓风洞中等离子体激励流动控制试验[J]. 航空学报, 2022, 43(S2): 89-96.
[7]	张旭东, 李铮, 董昊, 高思源, 纪祖赑, 黎凯昕, 白光辉. 高超声速流场等离子体逆向喷流减阻特性[J]. 航空学报, 2022, 43(S2): 115-123.
[8]	胡守超, 庄宇, 李贤, 江涛. 高超声速气动热标模HyHERM-Ⅰ试验[J]. 航空学报, 2022, 43(S2): 233-248.
[9]	李昊歌, 杨华, 杨雨欣, 陈伟芳. 高超声速升力体迎风面精细化降热优化设计[J]. 航空学报, 2022, 43(S2): 124-137.
[10]	吴东, 杨鸿, 赵文峰, 罗跃. 高超声速飞行器碳基结构高温应变测量[J]. 航空学报, 2022, 43(S2): 160-169.
[11]	聂春生, 袁野, 马伟, 曹占伟, 于明星. 主动引射气体参数对平板空气舵气动热影响[J]. 航空学报, 2022, 43(S2): 170-179.
[12]	马正雪, 罗振兵, 赵爱红, 周岩, 谢玮, 刘强, 朱寅鑫, 彭文强. 高超声速流场等离子体合成射流逆向喷流特性[J]. 航空学报, 2022, 43(S2): 192-203.
[13]	杨特, 杨智春, 梁舒雅, 康在飞, 贾有. 平稳随机载荷的信号特征提取与深度神经网络识别[J]. 航空学报, 2022, 43(9): 225952-225952.
[14]	刘传振, 孟旭飞, 刘荣健, 白鹏. 双后掠乘波体高超声速试验与数值分析[J]. 航空学报, 2022, 43(9): 126015-126015.
[15]	李珺, 王俊峰, 赵雅甜, 罗世彬. 面向非设计工况的激波针-喷流复合构型研究[J]. 航空学报, 2022, 43(9): 125949-125949.

高超声速飞行器气动弹性力学研究综述

Review of Studies on Aeroelasticity of Hypersonic Vehicles

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