Design and Response Characteristics Analysis of a Fast-response Sensor for Temperature and Heat Flux Measurement

doi:10.3969/j.issn.1000-1093.2014.06.026

Abstract

Abstract: A fast-response thermal resistance type heat flux sensor is designed to measure wall surface temperature and heat flux simultaneously in hypersonic vehicle long-time ground test. The thermocouple junctions are formed at the interfaces among different metal layers, and the heat flux and surface temperature could be achieved using the measured temperatures at the interfaces. A FEA model is built to simulate the internal heat transfer and response characteristics of the sensor. The numerical results show that theoretical assumptions could be met after a short-time response. The surface temperature and heat flux could be achieved simultaneously by considering temperature difference term and energy storing term during data reduction, and the effect of surface temperature on heat flux could be more closely reflected compared to the steady data reduction method.

Key words: test technology of aerocraft, heat flux sensor, heat flux measurement, surface temperature measurement, finite element analysis, response characteristics

CLC Number:

V441

YANG Qing-tao, BAI Han-chen, ZHANG Tao, YANG Juan, WANG Hui. Design and Response Characteristics Analysis of a Fast-response Sensor for Temperature and Heat Flux Measurement[J]. Acta Armamentarii, 2014, 35(6): 927-934.

References

［1］刘初平. 气动热与热防护试验热流测量［M］. 北京：国防工业出版社，2013.
LIU Chu-ping. Heat flux measurement in aerothermodynamics and thermal protection test［M］. Beijing: National Defense Industry Press, 2013.(in Chinese)
［2］陈连忠, 程梅莎, 洪文虎. 1 m电弧风洞大尺度防隔热组件烧蚀热结构试验［J］. 宇航材料工艺, 2009(6)：71-73.
CHEN Lian-zhong, CHENG Mei-sha, HONG Wen-hu. Ablation-thermal-structure test of large scale model in 1 m arc heated wind tunnel［J］. Aerospace Materials & Technology, 2009(6): 71-73. (in Chinese)
［3］江强, 周乐仪, 覃正,等. 液体碳氢燃料超燃冲压发动机支板凹槽稳焰技术试验［J］. 推进技术, 2011, 32(5): 680-683.
JIANG Qiang, ZHOU Le-yi, QIN Zheng, et al. Experimental investigation of strut-cavity flameholder technology in liquid hydrocarbon fueled scramjet combustor［J］. Journal of Propulsion Technology, 2011, 32(5): 680-683. (in Chinese)
［4］郭朝邦, 李文杰, 邢娅. 法国超燃冲压发动机主动冷却耐高温结构部件研究进展［J］. 飞航导弹, 2011(11): 84-91.
GUO Chao-bang, LI Wen-jie, XING Ya. Research advances in active cooling hot structure components of scramjet in france［J］. Aerodynamic Missile Journal, 2011(11): 84-91. (in Chinese)
［5］ ASTM E511-07 Standard test method for measuring heat flux using a copper-constantan circular foil, heat-flux transducer ［S］.
US: ASTM International, 2007.
［6］ Lee H J, Seung I S, Lee B J, et al. Heat flux measurement techniques over the protuberance at the hyper-sonic flow of Mach 7 ［C］∥16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.Bremen, Germany: AIAA, 2009: 19-22.
［7］ Chadwick K M. Stagnation heat transfer measurement techniques in hypersonic shock tunnel flows over spherical segments ［R］. Buffalo, New York: AIAA, 1997.
［8］ Lewis D R, Norris J D. Techniques for thin-skin heat-transfer measurements for surface roughness at AEDC tunnel 9 ［C］∥26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Seattle, Washington: AIAA, 2008: 23-26.
［9］ ASTM E422-99 Standard test method for mea- suring heat flux using a water-cooled calorimeter ［S］. US: ASTM International, 1999.
［10］ Kidd C T, Adams J J C. Fast-response heat-flux sensor for mea-surement commonality in hypersonic wind tunnels ［J］. Journal of Spacecraft and Rockets, 2001, 38(5): 719-729.
［11］ Raphael-Mabel S. Design and calibration of a novel high temperature heat flux sensor ［D］. Virginia: Virginia Polytechnic Institute and State University, 2005.
［12］ Roediger T, Knauss H, Estorf M, et al. Hypersonic instability waves measured using fast-response heat-flux gauges ［J］. Journal of Spacecraft and Rockets, 2009, 46(2): 266-273.
［13］ Liebert C H, Kolodziej P. Dual active surface heat flux gage probe ［C］∥41st International Instrumentation Symposium. Denver, Colorado: Instrument Society of America, 1995:7-11.
［14］李龙，范学军，王晶. 高温壁面热流与温度一体化测量传感器研究［J］. 实验流体力学, 2012, 26(2): 93-99.
LI Long, FAN Xue-jun, WANG Jing. Study of integrated high temperature sensor for wall heat flux and temperature measurements［J］. Journal of Experiments in Fluid Mechanics, 2012, 26(2): 93-99. (in Chinese)
［15］涂建强, 刘德英, 陈海群. 长时间隔热材料环境的稳态热流测量方法［J］. 宇航材料工艺, 2008(2): 76-80.
TU Jian-qiang, LIU De-ying, CHEN Hai-qun. Steady-state heat-flux measurement method for environment of long-time insulation materials ［J］. Aerospace Materials & Technology, 2008(2): 76-80. (in Chinese)
［16］ Hubble D O, Diller T E. A hybrid method for measuring heat flux［J］. Journal of Heat Transfer, 2010, 132(3)：031602.
［17］胡芃, 陈则韶. 量热技术和热物性测定［M］. 第2版. 合肥: 中国科技大学出版社, 2009.
HU Fan, CHEN Ze-shao. Calorimetry technology and thermal physical property measurement［M］. 2nd ed. Hefei: University of Science and Technology of China Press, 2009. (in Chinese)
［18］ Incropera F P, DeWitt D P, Bergman T L, et al. 传热和传质基本原理［M］. 第6版. 叶宏,葛新石, 徐斌，译. 北京: 化学工业出版社, 2009.
Incropera F P, DeWitt D P, Bergman T L, et al. Fundermantals of heat and mass transfer［M］. 6th ed. YE Hong， GE Xin-shi, XU Bin, Translated. Beijing: Chemistry Industry Press, 2009. (in Chinese)
［19］杨庆涛，白菡尘，杨娟. 薄壁量热计后壁面导热损失的影响及修正［C］∥第四届高超声速科技学术会议. 海南三亚: 中国力学学会，中国科学院高超声速科技中心，中国科学院力学研究所，高温气体动力学国家重点实验室，2011.
YANG Qing-tao, BAI Han-chen, YANG Juan. Influence and error correction due to heat conduction loss of thin-skin calorimeter back surface［C］∥4th Hypersonic Science and Technology Conference. Sanya, Hainan. The Chinese Society of Theoretical and Applied Mechanics, Hypersonic Research Center, CAS, Institute of Mechanics, CAS, State Key Laboratory of High Temperature Gas, 2011. (in Chinese)
［20］ Moaveni S. 有限元分析——ANSYS理论与应用［M］. 欧阳宇, 王崧,译. 北京: 电子工业出版社, 2003.
Moaveni S. Finite element analysis—ANSYS theory and application ［M］. OUYANG Yu, WANG Song, translated. Beijing: Publishing House of Electronics Industry, 2003. (in Chinese)

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