Research progress of aerothermoelasticity of air-breathing hypersonic vehicles

YANG Chao; ZHAO Huangda; WU Zhigang

doi:10.13700/j.bh.1001-5965.2019.0120

Volume 45 Issue 10

Oct. 2019

Turn off MathJax

Article Contents

Journal of Beijing University of Aeronautics and Astronautics > 2019 > 45(10): 1911-1923.

YANG Chao, ZHAO Huangda, WU Zhiganget al. Research progress of aerothermoelasticity of air-breathing hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(10): 1911-1923. doi: 10.13700/j.bh.1001-5965.2019.0120(in Chinese)

Citation:

YANG Chao, ZHAO Huangda, WU Zhiganget al. Research progress of aerothermoelasticity of air-breathing hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(10): 1911-1923. doi: 10.13700/j.bh.1001-5965.2019.0120(in Chinese)

Citation:

PDF( 5684 KB)

Research progress of aerothermoelasticity of air-breathing hypersonic vehicles

doi: 10.13700/j.bh.1001-5965.2019.0120

YANG Chao^{1, 2},
ZHAO Huangda^{1, 2},
WU Zhigang^{1, 2
,
,}

1.
School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China
2.
Key Laboratory of Aircraft Advanced Design Technology, Ministry of Industry and Information Technology, Beijing 100083, China

More Information

Corresponding author: WU Zhigang, E-mail: wuzhigang@buaa.edu.cn
Received Date: 22 Mar 2019
Accepted Date: 27 May 2019
Publish Date: 20 Oct 2019

Abstract

Abstract

Nowadays the air-breathing hypersonic vehicles are focused on by the researchers of aeronautics and astronautics. This type of vehicle usually uses a scramjet engine and an integrated design method, which brings a series of aeroelastic problems. This paper first describes the research progress of integrated airframe/engine modeling of air-breathing hypersonic vehicles. Then the research status of aerothermoelastic dynamics is introduced from the aspects of aerothermoelastic/propulsion coupling, control system coupling and uncertainty analysis. The related aerothermoelastic experimental research is analyzed. Finally, several suggestions for the study of aerothermoelastic problems of air-breathing hypersonic vehicles are proposed.
- aeroelasticity,
- integrated design,
- scramjet engine,
- air-breathing hypersonic vehicles,
- control system coupling

FullText(HTML)

References(73)

References

[1]	FLAHERTY K W, ANDREWS K M, LISTON G W.Operability benefits of airbreathing hypersonic propulsion for flexible access to space[J].Journal of Spacecraft and Rockets, 2010, 47(2):280-287. doi: 10.2514/1.43750
[2]	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. http://d.old.wanfangdata.com.cn/Periodical/hkxb201001001 YANG C, XU Y, XIE C C.Review of studies on aeroelasticity of hypersonic vehicles[J].Acta Aeronautica et Astronautica Sinica, 2010, 31(1):1-11(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201001001
[3]	MCNAMARA J J, FRIEDMANN P P.Aeroelastic and aerothermoelastic analysis in hypersonic flow:Past, present, and future[J].AIAA Journal, 2011, 49(6):1089-1122. doi: 10.2514/1.J050882
[4]	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. doi: 10.2514/3.21349
[5]	唐硕, 张栋, 祝强军.吸气式高超声速飞行器推进系统耦合建模与分析[J].飞行力学, 2013, 31(3):244-249. http://d.old.wanfangdata.com.cn/Periodical/fxlx201303012 TANG S, ZHANG D, ZHU Q J.Coupling model and analysis for air-breathing hypersonic vehicle propulsion system[J].Flight Dynamics, 2013, 31(3):244-249(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/fxlx201303012
[6]	TORREZ S, SCHOLTEN N, MICKA D, et al.A scramjet engine model including effects of precombustion shocks and dissociation: AIAA-2008-4619[R].Reston, VA: AIAA, 2008.
[7]	TORREZ S, DRISCOLL J, BOLENDER M, et al.Effects of improved propulsion modelling on the flight dynamics of hypersonic vehicles: AIAA-2008-6386[R].Reston, VA: AIAA, 2008.
[8]	TORREZ S, DRISCOLL J, DALLE D, et al.Scramjet engine model MASIV: Role of mixing, chemistry and wave interaction: AIAA-2009-4939[R].Reston, VA: AIAA, 2009.
[9]	TORREZ S, DRISCOLL J, DALLE D, et al.Hypersonic vehicle thrust sensitivity to angle of attuack and mach number: AIAA-2009-6152[R].Reston, VA: AIAA, 2009.
[10]	KLOCK R, CESNIK C E.Aerothermoelastic simulation of air-breathing hypersonic vehicles[C]//55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference.Reston, VA: AIAA, 2014: 149.
[11]	DALLE D, FRENDREIS S, DRISCOLL J, et al.Hypersonic vehicle flight dynamics with coupled aerodynamic and reduced-order propulsive models: AIAA-2010-7930[R].Reston, VA: AIAA, 2010.
[12]	PINCKNEY S Z, WALTON J T.Program SRGULL: An advanced engineering model for the prediction of airframe-integrated subsonic/supersonic hydrogen combustion ramjet cycle performance: Nasp Tm-1120[R].Washington, D.C.: NASA, 1991.
[13]	LOCKWOOD M, PETLEY D, HUNT J, et al.Airbreathing hypersonic vehicle design and analysis methods[C]//34th Aerospace Sciences Meeting and Exhibit.Reston, VA: AIAA, 1996: 381.
[14]	RANEY D L, MCMINN J D, POTOTZKY A S.Impact of aeroelastic-propulsive interactions on flight dynamics of a hypersonic vehicle[J].Journal of Aircraft, 1995, 32(2):355-362. doi: 10.2514/3.46723
[15]	KEE R J, RUPLEY F M, MEEKS E, et al.CHEMKIN-Ⅲ: A FORTRAN chemical kinetics package for the analysis of gas-phase chemical and plasma kinetics: SAND 96-8216[R].Livermore, CA: Sandia National Laboratories, 1996.
[16]	叶正寅, 孟宪宗, 刘成, 等.高超声速飞行器气动弹性的近期进展与发展展望[J].空气动力学学报, 2018, 36(6):984-994. doi: 10.7638/kqdlxxb-2018.0060 YE Z Y, MENG X Z, LIU C, et al.Progress and prospects on aeroelasticity of hypersonic vehicles[J].Acta Aerodynamica Sinica, 2018, 36(6):984-994(in Chinese). doi: 10.7638/kqdlxxb-2018.0060
[17]	ASHLEY H.Piston theory—A new aerodynamic tool for the aeroelastician[J].Journal of the Aeronautical Sciences, 1956, 23(12):1109-1118. doi: 10.2514/8.3740
[18]	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. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=6180486 ZHANG W W, YE Z Y.Numerical method of aeroelasticity based on local piston theory[J].Chinese Journal of Theoretical and Applied Mechanics, 2005, 37(5):632-639(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=6180486
[19]	YATES JR E C, BENNETT R M.Analysis of supersonic-hypersonic flutter of lifting surfaces at angle of attack[J].Journal of Aircraft, 1972, 9(7):481-489. doi: 10.2514/3.59019
[20]	ECKERT E.Engineering relations for heat transfer and friction in high-velocity laminar and turbulent boundary-layer flow over surfaces with constant pressure and temperature[J].Transactions of the ASME, 1956, 78(6):1273-1283.
[21]	SPALDING D, CHI S W.The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer[J].Journal of Fluid Mechanics, 1964, 18(1):117-143. doi: 10.1017/S0022112064000088
[22]	CHAVEZ F, SCHMIDT D.An integrated analytical aeropropulsive/aeroelastic model for the dynamic analysis of hypersonic vehicles: AIAA-92-4567-CP[R].Reston, VA: AIAA, 1992.
[23]	BOLENDER M A, DOMAN D B.A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle: AIAA-2005-6255[R].Reston, VA: AIAA, 2005.
[24]	WILLIAMS T, BOLENDER M, DOMAN D, et al.An aerothermal flexible mode analysis of a hypersonic vehicle: AIAA-2006-6647[R].Reston, VA: AIAA, 2006.
[25]	华如豪, 叶正寅.吸气式高超声速飞行器多学科动力学建模[J].航空学报, 2015, 36(1):346-356. http://d.old.wanfangdata.com.cn/Periodical/hkxb201501027 HUA R H, YE Z Y.Multidisciplinary dynamics modeling and analysis of a generic hypersonic vehicle[J].Acta Aeronautica et Astronautica Sinica, 2015, 36(1):346-356(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201501027
[26]	SUDALAGUNTA P R, SULTAN C, KAPANIA R K, et al.Aeroelastic control-oriented modeling of an airbreathing hypersonic vehicle[J].Journal of Guidance, Control, and Dynamics, 2018, 41(5):1136-1149. doi: 10.2514/1.G002777
[27]	SACHAN K, PADHI R.A brief survey on six-degree-of-freedom modeling for air-breathing hypersonic vehicles[C]//5th IFAC Conference on Advances in Cortrol and Optimization of Dynamical Systems ACODS 2018.Schlossplotz: IFAC, 2018, 51(1): 492-497.
[28]	李惠峰, 薛松柏, 张冉.吸气式高超声速飞行器机体推进控制一体化建模方法研究[J].宇航学报, 2012, 33(9):1185-1194. http://d.old.wanfangdata.com.cn/Periodical/yhxb201209001 LI H F, XUE S B, ZHANG R.Research of modeling method based on integrated design for airframe-propulsion-control of AHV[J].Journal of Astronautics, 2012, 33(9):1185-1194(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/yhxb201209001
[29]	肖进, 完颜振海, 杨亮, 等.面向控制的高超声速飞行器一体化建模与分析[J].计算机仿真, 2017, 34(2):92-96. http://d.old.wanfangdata.com.cn/Periodical/jsjfz201702021 XIAO J, WANYAN Z H, YANG L, et al.Control-oriented integrated modeling and analysis of hypersonic vehicle[J].Computer Simulation, 2017, 34(2):92-96(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/jsjfz201702021
[30]	SCHMIDT D.Dynamics and control of hypersonic aeropropulsive/aeroelastic vehicles: AIAA-92-4326-CP[R].Reston, VA: AIAA, 1992.
[31]	RUDD L, PINES D.Integrated propulsion effects on dynamic stability and control of hypersonic vehicles: AIAA-2000-3826[R].Reston, VA: AIAA, 2000.
[32]	MIRMIRANI M, WU C, CLARK A, et al.Modeling for control of a generic airbreathing hypersonic vehicle: AIAA-2005-6256[R].Reston, VA: AIAA, 2005.
[33]	FIDAN B, KUIPERS M, IOANNOU P, et al.Longitudinal motion control of air-breathing hypersonic vehicles based on time-varying models: AIAA-2006-8074[R].Reston, VA: AIAA, 2006.
[34]	BOLENDER M A, DOMAN D B.Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle[J].Journal of Spacecraft and Rockets, 2007, 44(2):374-387. doi: 10.2514/1.23370
[35]	CULLER A, WILLIAMS T, BOLENDER M.Aerothermal modeling and dynamic analysis of a hypersonic vehicle: AIAA-2007-6395[R].Reston, VA: AIAA, 2007.
[36]	向锦武, 曾开春, 聂璐.考虑弹性影响的乘波体飞行动力学特性[J].北京航空航天大学学报, 2012, 38(10):1306-1310. https://bhxb.buaa.edu.cn/CN/abstract/abstract12414.shtml XIANG J W, ZENG K C, NIE L.Elastic effects on flight mechanics of waverider[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10):1306-1310(in Chinese). https://bhxb.buaa.edu.cn/CN/abstract/abstract12414.shtml
[37]	FIDAN B, MIRMIRANI M, IOANNOU P.Flight dynamics and control of air-breathing hypersonic vehicles: Review and new directions: AIAA-2003-7081[R].Reston, VA: AIAA, 2003.
[38]	PARKER J T, SERRANI A, YURKOVICH S, et al.Control-oriented modeling of an air-breathing hypersonic vehicle[J].Journal of Guidance, Control, and Dynamics, 2007, 30(3):856-869. doi: 10.2514/1.27830
[39]	CUI Y, CAI G, ZHANG S, et al.Control-oriented modeling and characteristic analysis of an airbreathing hypersonic vehicle[C]//2014 IEEE Chinese Guidance, Navigation and Control Conference.Piscataway, NJ: IEEE Press, 2014: 1180-1185.
[40]	DICKESON J, RODRIGUEZ A, SRIDHARAN S, et al.Control-relevant modeling, analysis, and design for scramjet-powered hypersonic vehicles: AIAA-2009-7289[R].Reston, VA, AIAA, 2009.
[41]	DUAN H, LI P.Progress in control approaches for hypersonic vehicle[J].Science China:Technological Sciences, 2012, 55(10):2965-2970. doi: 10.1007/s11431-012-5036-x
[42]	方洋旺, 柴栋, 毛东辉, 等.吸气式高超声速飞行器制导与控制研究现状及发展趋势[J].航空学报, 2014, 35(7):1776-1786. http://d.old.wanfangdata.com.cn/Periodical/hkxb201407002 FANG Y W, CHAI D, MAO D H, et al.Status and development trend of the guidance and control for air-breathing hypersonic vehicle[J].Acta Aeronautica et Astronautica Sinica, 2014, 35(7):1776-1786(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201407002
[43]	吴立刚, 安昊, 刘健行, 等.吸气式高超声速飞行器控制的最新研究进展[J].哈尔滨工业大学学报, 2016, 48(10):1-16. http://d.old.wanfangdata.com.cn/Periodical/hebgydxxb201610001 WU L G, AN H, LIU J X, et al.Recent progress in control of air-breathing hypersonic vehicles[J].Journal of Harbin Institute of Technology, 2016, 48(10):1-16(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hebgydxxb201610001
[44]	王勇, 张艳, 白辰, 等.吸气式高超声速飞行器制导与控制方法综述[J].兵器装备工程学报, 2017, 38(4):72-76. http://d.old.wanfangdata.com.cn/Periodical/scbgxb201704016 WANG Y, ZHANG Y, BAI C, et al.Review of guidance and control approaches for air-breathing hypersonic vehicle[J].Journal of Ordnance Equipment Engineering, 2017, 38(4):72-76(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/scbgxb201704016
[45]	吴志刚, 楚龙飞, 杨超, 等.推力耦合的高超声速飞行器气动伺服弹性研究[J].航空学报, 2012, 33(8):1355-1363. http://d.old.wanfangdata.com.cn/Periodical/hkxb201208001 WU Z G, CHU L F, YANG C, et al.Study on aeroservoelasticity of hypersonic vehicles with thrust coupling[J].Acta Aeronautica et Astronautica Sinica, 2012, 33(8):1355-1363(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201208001
[46]	MCRUER D.Design and modeling issues for integrated airframe/propulsion control of hypersonic flight vehicles[C]//American Control Conference.Piscataway, NJ: IEEE Press, 1991: 729-734.
[47]	SERRANI A, ZINNECKER A M, FIORENTINI L, et al.Integrated adaptive guidance and control of constrained nonlinear air-breathing hypersonic vehicle models[C]//American Control Conference.Piscataway, NJ: IEEE Press, 2009: 3172-3177.
[48]	SCHMIDT D, VELAPOLDI J.Flight dynamics and feedback guidance issues for hypersonic airbreathing vehicles: AIAA-1999-4122[R].Reston, VA: AIAA, 1999.
[49]	HAO X, CHANG J, BAO W, et al.Preliminary design for coordinated control of airbreathing hypersonic vehicle and scramjet engine[C]//Proceedings of the 33rd Chinese Control Conference.Piscataway, NJ: IEEE Press, 2014: 909-914.
[50]	PETTIT C L.Uncertainty quantification in aeroelasticity:Recent results and research challenges[J].Journal of Aircraft, 2004, 41(5):1217-1229. doi: 10.2514/1.3961
[51]	BUSCHEK H, CALISE A.Robust control of hypersonic vehicles considering propulsive and aeroelastic effects: AIAA-1993-3762[R].Reston, VA: AIAA, 1993.
[52]	BUSCHEK H, CALISE A J.Uncertainty modeling and fixed-order controller design for a hypersonic vehicle model[J].Journal of Guidance, Control, and Dynamics, 1997, 20(1):42-48. doi: 10.2514/2.4031
[53]	CHAVEZ F, SCHMIDT D.Uncertainty modeling for large flexible high-speed aircraft: AIAA-1996-3920[R].Reston, VA: AIAA, 1996.
[54]	吴志刚, 杨超.气动伺服弹性系统不确定性建模与鲁棒稳定性[J].航空学报, 2003, 24(4):312-316. http://d.old.wanfangdata.com.cn/Periodical/hkxb200304006 WU Z G, YANG C.Modeling and Robust stability for aeroservoelastic systems with uncertainties[J].Acta Aeronautica et Astronautica Sinica, 2003, 24(4):312-316(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb200304006
[55]	曲鑫, 李菁菁, 宋勋, 等.考虑推进和气动弹性影响的高超飞行器的建模与控制[J].宇航学报, 2011, 32(2):303-309. http://d.old.wanfangdata.com.cn/Periodical/yhxb201102011 QU X, LI J J, SONG X, et al.Modeling and robust coupled control of air-breathing hypersonic vehicle considering propulsion and aeroelastic effects[J].Journal of Astronautics, 2011, 32(2):303-309(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/yhxb201102011
[56]	曾开春, 向锦武.高超声速飞行器飞行动力学特性不确定分析[J].航空学报, 2013, 34(4):798-808. http://d.old.wanfangdata.com.cn/Periodical/hkxb201304009 ZENG K C, XIANG J W.Uncertainty analysis of flight dynamic character for hypersonic vehicles[J].Acta Aeronautica et Astronautica Sinica, 2013, 34(4):798-808(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201304009
[57]	PU Z, TAN X, FAN G, et al.Uncertainty analysis and robust trajectory linearization control of a flexible air-breathing hypersonic vehicle[J].Acta Astronautica, 2014, 101:16-32. doi: 10.1016/j.actaastro.2014.01.025
[58]	MORGAN G H, MILLER W R.Flutter tests of some simple models at a Mach number of 7.2 in helium flow: NASA-MEMO-4-8-59L, L-199[R].Washington, D.C.: NASA, 1959.
[59]	HARRIS T M, HUTTSELL L J.Aeroelasticity research at wright-patterson air force base (wright field) from 1953-1993[J].Journal of Aircraft, 2003, 40(5):813-819. doi: 10.2514/2.6872
[60]	季辰, 李锋, 刘子强.高超声速风洞颤振试验技术研究[J].实验流体力学, 2015, 29(4):75-80. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=ltlxsyycl201504011 JI C, LI F, LIU Z Q.Research on flutter test technique in hypersonic wind tunnel[J].Journal of Experiments in Fluid Mechanics, 2015, 29(4):75-80(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=ltlxsyycl201504011
[61]	季辰, 赵玲, 朱剑, 等.高超声速风洞连续变动压舵面颤振试验[J].实验流体力学, 2017, 31(6):37-44. http://d.old.wanfangdata.com.cn/Periodical/ltlxsyycl201706006 JI C, ZHAO L, ZHU J, et al.Hypersonic wind tunnel flutter test research on rudder models by continuously varying dynamic pressure[J].Journal of Experiments in Fluid Mechanics, 2017, 31(6):37-44(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/ltlxsyycl201706006
[62]	韩景龙, 宣传伟, 张兵, 等.高超声速颤振数值与实验研究[C]//第十五届全国空气弹性学术交流会, 2017. HAN J L, XUAN C W, ZHANG B, et al.Numerical and experimental study of hypersonic flutter[C] //15th National Aeroelastic Academic Conference, 2017(in Chinese).
[63]	许辉.高超声速舵面颤振风洞试验与数值模拟影响因素研究[D].合肥: 合肥工业大学, 2018. XU H.Study on hypersonic control surface flutter wind tunnel test and it's numerical simulation[D].Heifei: Heifei University of Technology, 2018(in Chinese).
[64]	张红英, 孙姝, 程克明, 等.进气道工作状态对吸气式高超声速飞行器气动力特性影响的实验研究[J].宇航学报, 2007, 28(6):1488-1493. http://d.old.wanfangdata.com.cn/Periodical/yhxb200706010 ZHANG H Y, SUN S, CHENG K M, et al.Experimental investigation of inlet start unstart influences on the aerodynamic characteristic of a hypersonic vehicle[J].Journal of Astronautics, 2007, 28(6):1488-1493(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/yhxb200706010
[65]	张红英, 程克明, 伍贻兆.某高超飞行器流道冷流特征及气动力特性研究[J].空气动力学学报, 2009, 27(1):119-123. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb200901022 ZHANG H Y, CHENG K M, WU Y Z.A study on the flowpath and the aerodynamic characteristic of a hypersonic vehicle[J].Acta Aerodynamica Sinica, 2009, 27(1):119-123(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb200901022
[66]	姚文秀, 雷麦芳, 杨耀栋, 等.高超声速乘波飞行器气动实验研究[J].宇航学报, 2002, 23(6):82-85. http://d.old.wanfangdata.com.cn/Periodical/yhxb200206015 YAO W X, LEI M F, YANG Y D, et al.An aerodynamic experiment research of the hypersonic waverider vehicle[J].Journal of Astronautics, 2002, 23(6):82-85(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/yhxb200206015
[67]	吴颖川, 贺元元, 贺伟, 等.吸气式高超声速飞行器机体推进一体化技术研究进展[J].航空学报, 2015, 36(1):245-260. http://d.old.wanfangdata.com.cn/Periodical/hkxb201501020 WU Y C, HE Y Y, HE W, et al.Progress in airframe-propulsion integration technology of air-breathing hypersonic vehicle[J].Acta Aeronautica et Astronautica Sinica, 2015, 36(1):245-260(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/hkxb201501020
[68]	徐大军, 蔡国飙, 乐川.吸气式高超声速飞行器气动热试验研究[J].宇航学报, 2006, 27(5):1004-1009. http://d.old.wanfangdata.com.cn/Periodical/yhxb200605037 XU D J, CAI G B, LE C.Aeroheating experiment for airbreathing hypersonic vehicle[J].Journal of Astronautics, 2006, 27(5):1004-1009(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/yhxb200605037
[69]	HANK J, MURPHY J, MUTZMAN R.The X-51A scramjet engine flight demonstration program: AIAA-2008-2540[R].Reston, VA: AIAA, 2008.
[70]	WU Z G, CHU L F, YUAN R Z, et al.Studies on aeroservoelasticity semi-physical simulation test for missiles[J].Science China-Technological Sciences, 2012, 55(9):2482-2488. doi: 10.1007/s11431-012-4940-4
[71]	胡巍, 杨智春, 谷迎松.带操纵面机翼气动弹性地面试验仿真系统中的气动力降阶方法[J].西北工业大学学报, 2013, 31(5):810-815. http://d.old.wanfangdata.com.cn/Periodical/xbgydxxb201305025 HU W, YANG Z C, GU Y S.A new and effective method for Reducing order of aerodynamics of a wing with control surface for ground flutter test[J].Journal of Northwestern Polytechnical University, 2013, 31(5):810-815(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/xbgydxxb201305025
[72]	陈帅, 杨智春, 李斌.结构试验中均布载荷的气囊加载系统设计方法[J].工程力学, 2012, 29(6):146-150. http://www.cnki.com.cn/Article/CJFDTotal-GCLX201206022.htm CHEN S, YANG Z C, LI B.Design method of uniform loading system using airbags in structure test[J].Engineering Mechanic, 2012, 29(6):146-150(in Chinese). http://www.cnki.com.cn/Article/CJFDTotal-GCLX201206022.htm
[73]	侯英昱, 付志超, 朱剑, 等.气动力模拟非接触式加载方法研究[J].空气动力学学报, 2018, 36(2):357-361. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201802022 HOU Y Y, FU Z C, ZHU J, et al.Research on contactless loading method for aerodynamic force test[J].Acta Aerodynamica Sinica, 2018, 36(2):357-361(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201802022

Relative Articles

Supplements(0)

Cited By

Proportional views

Proportional views

通讯作者: 陈斌, bchen63@163.com

1.
沈阳化工大学材料科学与工程学院沈阳 110142

Figures(24)

Get Citation

PDF

XML

Article Metrics

Article views(1056) PDF downloads(563)

Research progress of aerothermoelasticity of air-breathing hypersonic vehicles

doi: 10.13700/j.bh.1001-5965.2019.0120

Abstract

References

Proportional views

Catalog

通讯作者: 陈斌, bchen63@163.com

Article Metrics

Proportional views

Related

Research progress of aerothermoelasticity of air-breathing hypersonic vehicles

doi: 10.13700/j.bh.1001-5965.2019.0120

Abstract

References

Proportional views

Catalog

通讯作者: 陈斌, bchen63@163.com

Article Metrics

Proportional views

Related

Export File

Citation

Format

Content