Combined thermal phenomena issues of long endurance hypersonic vehicles

GUI Yewei; LIU Lei; WEI Dong

doi:10.7638/kqdlxxb-2020.0078

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Combined thermal phenomena issues of long endurance hypersonic vehicles

更新时间：2026-05-28

- Combined thermal phenomena issues of long endurance hypersonic vehicles
- Vol. 38, Issue 4, Pages: 641-650(2020)
- 作者机构：
  
  中国空气动力研究与发展中心空气动力学国家重点实验室,绵阳,621000
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2020.0078
  CLC： V211.3
- Published：2020
- 稿件说明：
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桂业伟, 刘磊, 魏东. 长航时高超声速飞行器的综合热效应问题[J]. 空气动力学学报, 2020, 38(4): 641-650.

GUI Yewei, LIU Lei, WEI Dong. Combined thermal phenomena issues of long endurance hypersonic vehicles[J]. 2020, 38(4): 641-650.
桂业伟, 刘磊, 魏东. 长航时高超声速飞行器的综合热效应问题[J]. 空气动力学学报, 2020, 38(4): 641-650. DOI： 10.7638/kqdlxxb-2020.0078.

GUI Yewei, LIU Lei, WEI Dong. Combined thermal phenomena issues of long endurance hypersonic vehicles[J]. 2020, 38(4): 641-650. DOI： 10.7638/kqdlxxb-2020.0078.

摘要

针对长航时高超声速飞行器，分析了气动力/热与结构响应耦合情况下，结构受热变形带来的综合热效应问题。讨论了加热量与温度的关系，指出了在经过长时间加热后温度趋向于稳定时，温度分布特性仍然对结构热安全具有重要意义；明确了用辐射模拟气动加热来进行大面积结构热响应研究的实验途径。论文还讨论了在长时间加热情况下的一些综合热效应问题，明确了在优化设计中要考虑变形带来的对布局和轨道控制的系统性影响；讨论了在耦合实验测量中需要研究发展的技术问题；指出了长航时飞行中热量管理需要关注的几何和物理量多尺度问题。对这些问题的讨论与展望，将对下一步深化长航时高超声速飞行器的热防护和其他相关问题的耦合研究提供参考。

Abstract

The combined thermal phenomena of long endurance hypersonic vehicles

which are a series of multi-factor coupling phenomena resulted from the structural thermal response under the aerodynamic heating

are reviewed and prospected in this paper. The multi-factor phenomena are concerned with aerodynamic force/heating

thermal response of the vehicle structure

flight-orbit/control. As the relevancy of the heating to the temperature of the vehicle is analyzed

the characteristics of the steady temperature distribution are still significant to the thermal safety of the structure when the flight is on the long-time cruise. And the experimental method

that the aerodynamic heating is simulated by infrared radiation

is introduced for the heating test in large area structure. Based on the discussion about the combined thermal phenomena under long-time-heating

the systemic effects of thermal deformation on the configuration optimization and flight-orbit/flight-control design are suggested to be taken into account; some technical issues are proposed in the coupling experiment of thermal protection; and the geometrical and physical multi-scale analysis are discussed in the thermal management of the long endurance vehicles.

关键词

Keywords

references

HUANG W, LUO S B, WANG Z G. Key techniques and prospect of near-space hypersonic vehicle[J]. Journal of Astronautics, 2010, 31(5):1259-1265. (in Chinese)

魏毅寅, 刘鹏, 张冬青, 等.国外高超声速技术发展及飞行试验情况分析[J].飞航导弹, 2010, 5:2-9.

YANG Q, XIE W H, PENG Z J, et al. New concepts and trends in development of thermal protection design and analysis technology[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9):2981-2991. (in Chinese)

GUI Y W, TANG W, DU Y X, et al. Thermal safety issues of near-space hypersonic vehicles[M]. Beijing:National Defense Industry Press, 2019. (in Chinese)

GOGU C, BAPANAPALLI S K, HAFTKA R T, et al. Comparison of materials for an integrated thermal protection system for spacecraft reentry[J]. Journal of Spacecraft and Rockets, 2009, 46(3):501-513.

GEE D J, SIPCIC S R. Coupled thermal model for nonlinear panel flutter[J]. AIAA Journal, 1999, 37(5):642-650.

CHEN Y K, MILOS F S. Solution strategy for thermal response of nonablating thermal protection systems at hypersonic speeds[R]. AIAA-1996-0615.

CULLER A J, MCNAMARA J J. Fluid-thermal-structural modeling and analysis of hypersonic structures under combined loading[C]//52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, Colorado, 2011.

TRAN H, FARHAT C. An integrated platform for the simulation of fluid-structure-thermal interaction problems[C]//43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver, Colorado, 2002.

HAUPT M C, NIESNER R, UNGER R, et al. Computational aero-structural coupling for hypersonic applications[C]//9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, San Francisco, California, 2006.

HUANG T, MAO G L, JIANG G Q, et al. Two dimensional coupled flow-thermal-structural numerical simulation[J]. Acta Aerodynamica Sinica, 2000, 18(1):115-119. (in Chinese)

GENG X R, ZHANG H X, SHEN Q, et al. Study on an integrated algorithm for the flow fields of high speed vehicles and the heat transfer in solid structures[J]. Acta Aerodynamica Sinica, 2002, 20(4):422-427. (in Chinese)

GUI Y W, CHEN L, YU Z C, et al. The numerical simulation of coupled unsteady ablation and heat transfer in the porthole[J]. Journal of Engineering Thermophysics. 1997, 18(3):331-335. (in Chinese)

高晓成, 宁勇, 桂业伟, 等.高超声速球头外流场及其热响应的耦合计算[C]//第十届全国高超声速气动力热学术交流会, 云南: 1999.

LIU L, GUI Y W, GENG X R, et al. Study on the temperature field of hypersonic vehicle structure with aerothermoelasticity[J]. Acta Aerodynamica Sinica, 2015, 33(1):31-36. (in Chinese)

LIU S S, GUI Y W TANG W, et al. A new data transfer method in fluid-thermal-structure coupling problems[J]. Journal of Astronautics, 2016, 37(1):61-67. (in Chinese)

GUI Y W, LIU L, DAI G Y, et al. Research status on hypersonic vehicle fluid-thermal-structural coupling and software development[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(7):020844. (in Chinese)

DAI G Y, ZENG L, LIU S S, et al. Prediction of flight trajectory considering fluid-thermal-structural coupling effect[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(12):122346. (in Chinese)

GUI Y W. Combined thermal phenomena of hypersonic vehicle[J]. Scientia Sinica Physica, Mechanica Astronomica, 2019, 49(11):114702. (in Chinese)

GNOFFO P A, WEILMUENSTER K J, HAMILTON H H. Computational aerothermodynamic design issues for hypersonic vehicles[J]. Journal of Spacecraft and Rockets, 1999, 36(1):21-43.

ZHANG H Y, ZONG W G, GUI Y W. Numerical investigation of flow in leading edge gap of hypersonic vehicle[J]. Journal of Astronautics, 2014, 35(8):893-900. (in Chinese)

QIU B, GUO Y J, ZHANG H Y, et al. Free stream parameters effects on vortexes and aerodynamic heating environment in thermal protection tile transverse gaps[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3):761-770. (in Chinese)

YANG X F, GUI Y W, TANG W, et al. Numerical simulation of catalysis characteristics and near-wall thermochemical behavior in high-temperature carbon-oxygen gas mixture[J]. Journal of Engineering Thermophysics, 2018, 39(10):2244-2250. (in Chinese)

YANG Q T, BAI H C, ZHANG T, et al. Effects of adiabatic structure on heat flux measurement using a slug calorimeter[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(5):92-98. (in Chinese)

YANG Q T, BAI H C, LIU J C. Heat conduction loss correction of thin-skin calorimeter on back surface for state-variable measurement[J]. Journal of Aerospace Power. 2015, 30(2):349-355. (in Chinese)

QU Z, WANG X, TANG Y L, et al. In situ visualization measurement of flat plate ablation in high-temperature gas flow[J]. Journal of Applied Mechanics, 2018, 85(6):061006.

WEI D, YANG X F, SHI Y A, et al. A method for reconstructing two-dimensional surface and internal temperature distributions in structures by ultrasonic measurements[J]. Renewable Energy. 2020.150:1108-1117.

XIA L S, QI B, TIAN N, et al. Study on modeling analysis and testing method of electro-thermal properties of quartz lamp[J]. Infrared Technology, 2015, 37(10):877-882. (in Chinese)

KONG F J, ZHANG W, WU Z Q, et al. Study on electro-thermal properties of quartz-lamp element for the thermal-structural test[J]. Structure Environment Engineering, 2012, 39(4):1-6. (in Chinese)

ZHU Y D, LIU X, ZENG L, et al. Optimization design of aerodynamic heating of large area simulated by quartz lamp array[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(9):520981. (in Chinese)

ZHU Y D, WEI D, LIU S S, et al. Power optimization of non-uniform aerodynamic heating simulated by quartz lamp array[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(6):122761. (in Chinese)

ROGER M. Aerothermoelasticity[J]. Aero Space Engineering, 1958, 17(10):34-43, 64.

GUO J, ZHANG Z, WANG J M, et al. Study on nonlinear aeroelastic response of panel structure based on classical and local piston theories[J]. Structure Environment Engineering, 2018, 45(5):7-12. (in Chinese)

XIN J Q, QU Q, XU X J, et al. Aerothermoelastic analysis method of hypersonic vehicle rudder[J]. Structure Environment Engineering, 2015, 42(3):1-9. (in Chinese)

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):983-994. (in Chinese)

ZHANG Y, LI W J, TANG W, et al. Aerodynamic shape optimization of reentry body using Pareto genetic algorithm[J]. Acta Aerodynamica Sinica, 2001, 19(4):478-482. (in Chinese)

TANG W, GUI Y W, FANG F. Aerodynamic configurations selection for lift reentry capsule[J]. Journal of Astronautics, 2008, 29(1):84-88. (in Chinese)

CHE J, TANG S, HE K F. Research on aerodynamic configuration optimization of integral performance for hypersonic cruise vehicle[J]. Acta Aerodynamica Sinica, 2009, 27(2):214-219. (in Chinese)

TANG W, GUI Y W, WANG A L. Proposal of thermal configuration optimization design for a maneuverable vehicle[J]. Journal of Astronautics, 2009, 30(5):1803-1807. (in Chinese)

DAI G Y, JIA H Y, ZENG L, et al. Effects of fluid-thermal-structural coupling on inlet parameters of hypersonic intake[J]. Journal of Propulsion Technology, 2018, 39(6):1267-1274. (in Chinese)

WEI D, SHI Y A, YANG X F, et al. Lightweight design method of thermal protection tile for hypersonic vehicle based on variable thickness[J]. Journal of Astronautics, 2018, 39(3):285-291. (in Chinese)

WANG P G, LIU Y G, WANG J. Discussion on integrated environment control/thermal management system concepts for hypersonic vehicle[J]. Engineering Science, 2007, 9(2):44-48. (in Chinese)

MA W, XUAN Y M, HAN Y G. Thermal management and design principles of stratospheric vehicles[J]. Journal of Astronautics, 2009, 30(5):2092-2096. (in Chinese)

DU Y X, XIAO G M, GUI Y W, et al. Heat transfer characteristics of phase-change thermal control unit[J]. CIESC Journal, 2012, 63(S1):107-113. (in Chinese)

DU Y X, XIAO G M, GUI Y W, et al. Study on heat transfer characteristics of phase-change energy storage unit for thermal management[J]. International Journal of Thermophysics. 2014, 35(8):1577-1589.

WU N N, KANG H L, LUO J L. Experimental study on fine thermal measurement of high-speed aircraft wing rudder gap in shock wave tunnel[J]. Acta Aerodynamica Sinica, 2019, 37(1):133-139. (in Chinese)

ZHU G S, NIE C S, CAO Z W, et al. Research progress of aerodynamic thermal environment test and measurement technology[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(2):1-10. (in Chinese)

ZHU C, CHEN D J, ZHOU W, et al. Evaluation of arc-heated wind-tunnel operation in CO 2 atmosphere[J ] . Journal of Experiments in Fluid Mechanics, 2015, 29(1):31-36. (in Chinese)

WU D, CHEN D J, ZHOU W, et al. High temperature strain measurement of the front edge structure in high thermal environment[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(3):92-97. (in Chinese)

王振峰, 李向东, 王铁军.高超声速压缩楔气动力/热/结构耦合试验模型设计及测试方案研究[C]//第十八届全国高超声速气动力热学术交流会, 杭州: 2016.

LIU L, DAI G Y, ZENG L, et al. Preliminary test model design of fluid-thermal-structural interaction problems[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(11):221165. (in Chinese)

LIU L, DAI G Y, ZENG L, et al. Experimental model design and preliminary numerical verification of fluid-thermal-structural coupling problem[J]. AIAA Journal, 2019:1715-1724.

ZHAO J S, ZHANG Z G, SHI Y L, et al. Research on the conversion method of aeroheating environment of hypersonic vehicle[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(5):1235-1243. (in Chinese)

GONG A L, XIE J, LIU X W, et al. Study on ground-to-flight extrapolation of near space hypersonic aerodynamic data[J]. Engineering Mechanics, 2017, 34(10):229-238. (in Chinese)

LIU L. Study on the characteristics and similarity criteria of aerothermoelasticity for hypersonic vehicle[D]. Mianyang: China Aerodynamics Research and Development Center, 2014. (in Chinese)

LIU L, GUI Y W, DU Y X, et al. Study on the similarity criteria of aircraft thermal protection structures[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(3):25-29. (in Chinese)

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