高超声速全动翼面全时域耦合分析方法及应用

doi:10.7527/S1000-6893.2021.25773

Abstract

Abstract: Based on the synchronous method of flow-structure temperature field, a multi field full-time coupling method is established for the aerothermoelastic stability and transient response analysis of a hypersonic all-movable wing along the trajectory. The aerothermal synchronization algorithm is used to simulate the hypersonic flow and the structural temperature field. The interpolation methods of aerodynamic and the structure temperature field are established. The non-inertial frame of reference describing the attitude, and the dynamic grids methods describing the wing vibration are superimposed by coordinate transformation. The coupling unsteady effect of the attitude and vibration of the all-movable wing is considered. Finally, an aerothermoelastic stability analysis method combining synchronization algorithm with full-time coupling method is established. The present method is applied to the thermal flutter prediction and transient response analysis of a hypersonic all-movable wing operating along a given trajectory. It is found that due to the influence of structural vibration, fluctuation amplitude of heat flux at the monitoring point accounts for about 10% of the peak, while temperature decreased about 0.3%. A coupled bending-torsion flutter is obtained by the full-time coupling method is between the 4-5 trajectory state points, which is consistent with the results of the "modal freezing" thermal flutter method.

Key words: hypersonic, all-movable wing, full-time coupling, aerothermoelastic, unsteady, flutter

CLC Number:

V215.3

SHEN Ennan, GUO Tongqing, WU Jiangpeng, HU Jialiang, ZHANG Guijiang. Full-time coupling method and application of a hypersonic all-movable wing[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525773-525773.

References

[1] LIVNE E, WEISSHAAR T A. Aeroelasticity of nonconventional airplane configurations-past and future[J].Journal of Aircraft, 2003, 40(6):1047-1065.
[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 YANG C,XU Y, XIE C C. Review of studies on aeroelasticity of hypersonic veicles.[J] Acta Aeronautica et Astronautica Sinica, 2010,31(1):1-11(in Chinese).
[3] KLOCK R, CESNIK C E. Aerothermoelastic reduced-order model of a hypersonic vehicle[C]//AIAA Atmospheric Flight Mechanics Conference. Reston:AIAA, 2015.
[4] MCNAMARA J, FRIEDMANN P, POWELL K, et al. Three-dimensional aeroelastic and aerothermoelastic behavior in hypersonic flow[C]//46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Reston:AIAA, 2005.
[5] MCNAMARA J J, FRIEDMANN P P, POWELL K G, et al. Aeroelastic and aerothermoelastic behavior in hypersonic flow[J].AIAA Journal, 2008, 46(10):2591-2610.
[6] LV J, WANG F, GUO L, et al. CFD/CSD approach to predict hypersonic aerothermoelastic response of a wing[J].Procedia Engineering, 2015, 126:123-127.
[7] YE K, YE Z, ZHANG Q, et al. Study on areothermoelastic for hypersonic all moving control surface[C]//International Bhurban Conference on Applied Sciences and Technology.Piscataway:IEEE Press, 2016:467-475.
[8] GUO T Q, SHEN E N,LU Z L, et al. Thermal flutter prediction at trajectory points of a hypersonic vehicle based on aerothermal synchronization algorithm[J].Aerospace Science and Tecnology, 2019, 94:105381.
[9] 张伟伟, 夏巍, 叶正寅. 一种高超音速热气动弹性数值研究方法[J].工程力学, 2006, 23(2):41-46. ZHANG W W, XIA W, YE Z Y. A numerical method for hypersonic aerothermoelasticity[J].Engineering Mechanics, 2006, 23(2):41-46(in Chinese).
[10] 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 Z G, HUI J P, YANG C. Hypersonic aerothermoelastic analysis of wings[J].Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(3):270-273(in Chinese).
[11] 史晓鸣, 杨炳渊. 瞬态加热环境下变厚度板温度场及热模态分析[J].计算机辅助工程, 2006, 15(b09):15-18. SHI X M, YANG B Y. Temperature field and mode analysis of flat plate with thermal environment of transient heating[J].Computer Aided Engineering, 2006, 15(b09):15-18(in Chinese).
[12] 叶献辉, 杨翊仁. 三维壁板热颤振分析[J].振动与冲击, 2008, 27(6):55-59. YE X H, YANG Y R. Thermal flutter analysis of a three-dimension panel[J].Journal of Vibration and Shock, 2008, 27(6):55-59(in Chinese).
[13] 吴振强, 程昊, 张伟,等. 热环境对飞行器壁板结构动特性的影响[J].航空学报, 2013, 34(2):334-342. WU Z Q, CHENG H, ZHANG W, et al. Effects of thermal environment on dynamic properties of aerospace vehicle panel structures[J].Acta Aeronautica et Astronautica Sinica, 2013, 34(2):334-342(in Chinese).
[14] 王宏宏, 陈怀海, 崔旭利,等. 热效应对导弹翼面固有振动特性的影响[J].振动、测试与诊断, 2010, 30(3):275-279. WANG H H, CHEN H H, CUI X L et al. Thermal effect on dynamic characteristics of a missile wing[J].Journal of Vibration, Measurement & Diagnosis, 2010, 30(3):275-279(in Chinese).
[15] 杨享文, 武洁, 叶坤,等. 高超声速全动舵面的热气动弹性研究[J].力学学报, 2014, 46(4):626-630. YANG X W, WU J, YE K,et al. Study on aerothermoelasticity of a hypersonic all-movable control surface[J].Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(4):626-630(in Chinese).
[16] 刘成, 叶正寅, 叶坤. 转捩位置对全动舵面热气动弹性的影响[J].力学学报, 2017, 49(4):802-810. LIU C, YE Z Y, YE K. The effect of transition location on aerothermoelasticity of a hypersonic all-movable control surface[J].Chinese Journal of Theoretical and Applied Mechanics, 2017, 49(4):802-810(in Chinese).
[17] 谭光辉, 李秋彦, 冉玉国,等. 一种高超音速热颤振工程分析方法[C]//第十一届全国空气弹性学术交流会, 2009:34-37. TAN G H, LI Q Y, RAN Y G,et al.An engineer method for hypersonic flutter with thermal effects[C]//The 11th National Aeroelasticity Academic Conference, 2009:34-37(in Chinese).
[18] 李丽丽. 气动加热环境下壁板的颤振分析方法研究[D]. 南京:南京航空航天大学, 2012:7-57. LI L L. Thermal flutter analysis of panel under the aerodynamic heating environment[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012:7-57(in Chinese).
[19] 桂业伟,刘磊,耿湘人,等.气动力/热与结构多场耦合计算策略与方法研究[J].工程热物理学报,2015, 36(5):1047-1051. GUI Y W, LIU L, GENG X R,et al. Study on the computation strategy and method of aero-dynamic -thermal-structural coupling problem.[J] Journal of Engineering Thermophysics, 2015, 36(5):1047-1051(in Chinese).
[20] 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. YE Z Y,MENG X Z, LIU C, et al. Process and prospects on aeroelasticity of hypersonic vehicles[J].Acta Aerodynamica Sinica, 2018, 36(6):984-994(in Chinsese).
[21] 沈恩楠,陆志良,郭同庆,等.考虑空腔的高超声速多流动区域同步数值模拟[J].空气动力学学报,2019,37(6):931-937. SHEN E N, LU Z L, GUO T Q, et al. A synchronized method for multi-regional simulation in hypersonic flow with inclusion of convection in a contained cavity[J].Acta Aerodynamica Sinica, 2019, 37(6):931-937(in Chinese).

Full-time coupling method and application of a hypersonic all-movable wing

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Zhikun SUN, Zhiwei SHI, Weilin ZHANG, Zheng LI, Qijie SUN. Effect of plasma actuator on lift-drag characteristics of high-speed airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 23-39.
[2]	Weizhuo HUA, Ling GAO, Ge CHEN, Yiwen LI, Geng GONG, Yantao WANG, Biao WEI. Experimental magneto-hydrodynamic system based on plasma torch [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 1-7.
[3]	Yifeng HUANG, Shuhua ZENG, Zhongzheng JIANG, Weifang CHEN. Numerical study on high-altitude lateral jet based on nonlinear coupled constitutive relation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 8-22.
[4]	Kai LUO, Yonghai WANG, Qiu WANG, Jiwei LI, Zheng LI, Chunsheng NIE, Zheng LI. Plasma-actuated flow control test in high enthalpy shock tunnel [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 89-96.
[5]	Xudong ZHANG, Zheng LI, Hao DONG, Siyuan GAO, Zubi JI, Kaixin LI, Guanghui BAI. Drag reduction characteristics of opposing plasma synthetic jet in hypersonic flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 115-123.
[6]	Shouchao HU, Yu ZHUANG, Xian LI, Tao JIANG. Hypersonic aero-heating environment research model HyHERM-I: Experiment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 233-248.
[7]	Haoge LI, Hua YANG, Yuxin YANG, Weifang CHEN. Refinement optimization design for heat reduction on windward surface of hypersonic lifting body [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 124-137.
[8]	Dong WU, Hong YANG, Wenfeng ZHAO, Yue LUO. High temperature strain measurement of hypersonic aircraft carbon-based composite material structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 160-169.
[9]	Chunsheng NIE, Ye YUAN, Wei MA, Zhanwei CAO, Mingxing YU. Effect of active ejection gas parameters on thermal environment of plate and air rudder [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 170-179.
[10]	Zhengxue MA, Zhenbing LUO, Aihong ZHAO, Yan ZHOU, Wei XIE, Qiang LIU, Yinxin ZHU, Wenqiang PENG. Reverse jet characteristics of plasma synthetic jet in hypersonic flow field [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 192-203.
[11]	LIU Chuanzhen, MENG Xufei, LIU Rongjian, BAI Peng. Experimental and numerical investigation of hypersonic performance of double swept waverider [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 126015-126015.
[12]	LI Jun, WANG Junfeng, ZHAO Yatian, LUO Shibin. Research on combinational configuration of spike and multi-jets in off-design regimes [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 125949-125949.
[13]	WANG Yi, XU Shangcheng, ZHOU Yunfan, FAN Xiaoqiang, WANG Zhenguo. Multi-objective design and analysis of cowl lip angle for hypersonic inlet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125698-125698.
[14]	WU Qiang, XU Haojun, WEI Yang, PEI Binbin, XUE Yuan. Aerodynamics/flight dynamics coupling characteristics of aircraft under icing conditions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125566-125566.
[15]	ZHENG Hui, QIU Lei, YUAN Shenfang, YANG Xiaofei, LU Xulong, XUE Zhaopeng. Experimental method of guided wave monitoring for high temperature airflow damage of C/C thermal protection structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 225659-225659.