Volume 35 Issue 4
Aug.  2021
Turn off MathJax
Article Contents
ZHU X X,ZHU T,YANG K,et al. Development of small size Schmidt-Boelter heat flux sensor[J]. Journal of Experiments in Fluid Mechanics, 2021,35(4):106-111. doi: 10.11729/syltlx20200065
Citation: ZHU X X,ZHU T,YANG K,et al. Development of small size Schmidt-Boelter heat flux sensor[J]. Journal of Experiments in Fluid Mechanics, 2021,35(4):106-111. doi: 10.11729/syltlx20200065

Development of small size Schmidt-Boelter heat flux sensor

doi: 10.11729/syltlx20200065
  • Received Date: 2020-06-01
  • Rev Recd Date: 2020-07-20
  • Available Online: 2021-08-26
  • Publish Date: 2021-08-31
  • A kind of small size Schmidt-Boelter Gage was successfully developed for measuring heat flux in conventional hypersonic wind tunnel test. The simulation model of the Schmidt-Boelter Gage was built. The structure and size of the sensor were optimized based on the simulation model. According to the optimized results, the sensor with the size of Φ 3×10 mm was made and tested in the arc lamp heat flux calibration system. The results show that the size and performance of the developed sensor are comparable to the foreign sensor level. The sensitivity is greater than 30 μV·m2/kW, and the response time is about 50 ms.
  • loading
  • [1]
    陈坚强,涂国华,张毅锋,等. 高超声速边界层转捩研究现状与发展趋势[J]. 空气动力学学报,2017,35(3):311-337. doi: 10.7638/kqdlxxb-2017.0030

    CHEN J Q,TU G H,ZHANG Y F,et al. Hypersonic boundary layer transition: what we know, where shall we go[J]. Acta Aerodynamica Sinica,2017,35(3):311-337. doi: 10.7638/kqdlxxb-2017.0030
    [2]
    欧阳金栋,刘慧慧,邓进,等. 高超声速飞行器结构热防护技术现状综述[J]. 教练机,2017(1):39-43. doi: 10.3969/j.issn.1005-7420.2017.01.007

    OUYANG J D,LIU H H,DENG J,et al. Research status of structural thermo protection technology for hypersonic speeding missile[J]. Trainer,2017(1):39-43. doi: 10.3969/j.issn.1005-7420.2017.01.007
    [3]
    王璐,王友利. 高超声速飞行器热防护技术研究进展和趋势分析[J]. 宇航材料工艺,2016,46(1):1-6. doi: 10.3969/j.issn.1007-2330.2016.01.001

    WANG L,WANG Y L. Research progress and trend analysis of hypersonic vehicle thermal protection technology[J]. Aerospace Materials & Technology,2016,46(1):1-6. doi: 10.3969/j.issn.1007-2330.2016.01.001
    [4]
    孟松鹤,丁小恒,易法军,等. 高超声速飞行器表面测热技术综述[J]. 航空学报,2014,35(7):1759-1775. doi: 10.7527/S1000-6893.2013.0401

    MENG S H,DING X H,YI F J,et al. Overview of heat measurement technology for hypersonic vehicle surfaces[J]. Acta Aeronautica et Astronautica Sinica,2014,35(7):1759-1775. doi: 10.7527/S1000-6893.2013.0401
    [5]
    刘初平, 杨庆涛, 王辉, 等. 气动热与热防护试验热流测量[M]. 北京: 国防工业出版社, 2013.
    [6]
    韩曙光,贾广森,文帅,等. 磷光热图技术在常规高超声速风洞热环境实验中的应用[J]. 气体物理,2017,2(4):56-63. doi: 10.19527/j.cnki.2096-1642.2017.04.006

    HAN S G,JIA G S,WEN S,et al. Heat transfer measurement using a quantitative phosphor thermography system in blowdown hypersonic facility[J]. Physics of Gases,2017,2(4):56-63. doi: 10.19527/j.cnki.2096-1642.2017.04.006
    [7]
    毕志献,韩曙光,伍超华,等. 磷光热图测热技术研究[J]. 实验流体力学,2013,27(3):87-92.

    BI Z X,HAN S G,WU C H,et al. Phosphor thermography study ingun tunnel[J]. Journal of Experiments in Fluid Mechanics,2013,27(3):87-92.
    [8]
    张仕忠,李进平,张晓源,等. 一种新型瞬态量热计的研制[J]. 中国科学: 技术科学,2018,48(5):558-564. doi: 10.1360/N092017-00245

    ZHANG S Z,LI J P,ZHANG X Y,et al. Development of a novel transient calorimeter[J]. Scientia Sinica (Technologica),2018,48(5):558-564. doi: 10.1360/N092017-00245
    [9]
    曾磊,桂业伟,贺立新,等. 镀层式同轴热电偶数据处理方法研究[J]. 工程热物理学报,2009,30(4):661-664. doi: 10.3321/j.issn:0253-231X.2009.04.032

    ZENG L,GUI Y W,HE L X,et al. Study on data processing methods for coaxial-thermal-couple heat-flux sensor[J]. Journal of Engineer-ing Thermophysics,2009,30(4):661-664. doi: 10.3321/j.issn:0253-231X.2009.04.032
    [10]
    MATTHEWS R K, NUTT K W, WANNENWETSCH G D, et al. Developments in aerothermal test techniques at the AEDC supersonic-hypersonic wind tunnels[C]//Proc of the 20th Thermophysics Confe-rence. 1985. doi: 10.2514/6.1985-1003
    [11]
    NAKOS J T. Description of heat flux measurement methods used in hydrocarbon and propellant fuel fires at Sandia.[R]. SAND2010-7062, 2010. doi: 10.2172/1005030
    [12]
    KIDD C T, SCOTT W T. New techniques for transient heat-transfer measurement in hypersonic flow at the AEDC[C]//Proc of the 37th Aerospace Sciences Meeting and Exhibit. 1999. doi: 10.2514/6.1999-823
    [13]
    KIDD C T, ADAMS J C Jr. Development of a heat-flux sensor for commonality of measurement in AEDC hypersonic wind tunnels[C]//Proc of the 21st Aerodynamic Measurement Technology and Ground Testing Conference. 2000. doi: 10.2514/6.2000-2514
    [14]
    HOFFIE A F. Convection calibration of Schmidt-Boelter heat flux gages in shear and stagnation air flow[D]. Virginia: Virginia Polytech-nic Institute and State University, 2006.
    [15]
    Vatell Corporation. Certificate of calibration of Schmidt-Boelter heat flux trans ducer[Z]. Serial Number: 0118, Date calibrated: 10-09-2013.
    [16]
    罗浩,彭同江. 一种多级式热电堆型微量热流传感器的设计与制备[J]. 西南科技大学学报,2014,29(1):55-59. doi: 10.3969/j.issn.1671-8755.2014.01.012

    LUO H,PENG T J. Design and preparation of a multi-stage thermopile-type micro-heat flow flux sensor[J]. Journal of Southwest University of Science and Technology,2014,29(1):55-59. doi: 10.3969/j.issn.1671-8755.2014.01.012
    [17]
    储小刚. 热电堆式热流传感器的设计与实验研究[D]. 南京: 南京理工大学, 2016.

    CHU X G. Design and experimental study of thermoelectric heat flux sensor[D]. Nanjing: Nanjing University of Science and Technology, 2016. doi: 10.7666/d.Y3046258
    [18]
    石逸武,罗永祥,许喜銮,等. 硅油及填料对导热硅脂接触热阻的影响[J]. 电子与封装,2013,13(8):30-33. doi: 10.16257/j.cnki.1681-1070.2013.08.011

    SHI Y W,LUO Y X,XU X L,et al. Effect of silicone oil and filler on thermal resistance of thermal conductive grease[J]. Electronics & Packaging,2013,13(8):30-33. doi: 10.16257/j.cnki.1681-1070.2013.08.011
    [19]
    朱新新,杨庆涛,王辉,等. 塞块式量热计隔热结构的改进与试验分析[J]. 实验流体力学,2018,32(6):34-40. doi: 10.11729/syltlx20180071

    ZHU X X,YANG Q T,WANG H,et al. Improvement of heat insulation structure in the slug calorimeter and test analysis[J]. Journal of Experiments in Fluid Mechanics,2018,32(6):34-40. doi: 10.11729/syltlx20180071
    [20]
    MURTHY A V,TSAI B K,SAUNDERS R D. Radiative calibration of heat-flux sensors at NIST: facilities and techniques[J]. Journal of Research of the National Institute of Standards and Technology,2000,105(2):293-305. doi: 10.6028/jres.105.033
    [21]
    朱新新,王辉,杨庆涛,等. 弧光灯热流标定系统的光学设计[J]. 光学学报,2016,36(11):1122001. doi: 10.3788/AOS201636.1122001

    ZHU X X,WANG H,YANG Q T,et al. Optical design of arc lamp heat flux calibration system[J]. Acta Optica Sinica,2016,36(11):1122001. doi: 10.3788/AOS201636.1122001
    [22]
    杨凯,杨庆涛,朱新新,等. 一种薄膜热电堆热流传感器灵敏度系数的实验研究[J]. 宇航计测技术,2018,38(3):67-72. doi: 10.12060/j.issn.1000-7202.2018.03.11

    YANG K,YANG Q T,ZHU X X,et al. Calibration tests on a new thin-film thermopile heat-flux sensor[J]. Journal of Astronautic Metrology and Measurement,2018,38(3):67-72. doi: 10.12060/j.issn.1000-7202.2018.03.11
    [23]
    WANG H,YANG Q T,ZHU X X,et al. Inverse estimation of heat flux using linear artificial neural networks[J]. International Journal of Thermal Sciences,2018,132:478-485. doi: 10.1016/j.ijthermalsci.2018.04.034
  • 加载中

Catalog

    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

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(8)  / Tables(2)

    Article Metrics

    Article views (881) PDF downloads(69) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return