
北京大学 工学院,湍流与复杂系统国家重点实验室,北京,100871
Published:2024
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余港龙, 朱一丁. 基于光强方法的双层温敏漆点阵的热流密度测量[J]. 空气动力学学报, 2024, 42(6): 35−43.
YU Ganglong, ZHU Yiding. Light intensity based heat flux measurement with double-layer temperature-sensitive paint lattices[J]. 2024, 42(6): 35-43.
余港龙, 朱一丁. 基于光强方法的双层温敏漆点阵的热流密度测量[J]. 空气动力学学报, 2024, 42(6): 35−43. DOI: 10.7638/kqdlxxb-2023.0119
YU Ganglong, ZHU Yiding. Light intensity based heat flux measurement with double-layer temperature-sensitive paint lattices[J]. 2024, 42(6): 35-43. DOI: 10.7638/kqdlxxb-2023.0119.
为提高长时间热流密度测量的精度,提出了一种基于双层温敏漆点阵涂层的热流密度直测技术。该技术运用精细喷涂技术在厚度均匀的透明膜L2的上下表面分别喷涂错位分布的温敏漆点阵L3和L1。结合图像边缘检测和粒子图像测速的询问算法确定温敏漆点阵位置,提取温敏漆喷涂点的光强,由光强-温度标定关系可以测得L1和L3上的温度分布;分别采用Cook-Felderman方法和Fourier导热定律计算热流密度,并与热流密度传感器测量结果进行比较,结合热渗透时间分析不同方法的适用性。结果表明:双层温敏漆点阵方法既能用Cook-Felderman方法捕捉短时间热冲击下的瞬态热流密度,又能用Fourier导热定律测量长时间稳态的热流密度,在高速热流密度测量中有一定的应用前景。
An intensity-based method for direct heat flux measurement with double-layer temperature-sensitive paint (DL-TSP) lattices has been proposed in this study. With the aid of an accurate spray technique
temperature-sensitive paint lattices L3 and L1 are sprayed in a staggered arrangement on the upper and lower surfaces of a transparent film L2 of uniform thickness
respectively. Utilizing image edge detection and interrogation of particle image velocimetry (PIV) to locate the lattices
the light intensity of spray points of the temperature-sensitive paint can be extracted
and the corresponding temperature distributions of L1 and L3 can be obtained from the light intensity-temperature calibration relation. The heat flux is calculated using both the Cook-Felderman method and the Fourier’s law
which are compared with data from the heat flux sensor. The applicability of different methods is analyzed based on the thermal penetration time. The results indicate that the double-layer temperature-sensitive paint lattice method can not only capture the transient heat flux under short-term thermal shock using the Cook-Felderman method
but also measure the long-term steady-state heat flux using the Fourier’s law. The present method has certain application prospects in the heat flux measurement of high-speed flows.
LIU T S, CAMPBELL B T, SULLIVAN J P, et al . Heat transfer measurement on a waverider at Mach 10 using fluorescent paint[J ] . Journal of Thermophysics and Heat Transfer, 1995 , 9 ( 4 ): 605 − 611 .
LIU T S, SULLIVAN J P. Pressure and temperature sensitive paints[M]. Springer Verlag, 2005.
CAI Z M, LIU T S, MONTEFORT J . Numerical inverse method for calculating heat flux in temperature-sensitive-coating measurement on a finite base[J ] . International Journal of Heat and Mass Transfer, 2018 , 127 : 1099 − 1113 .
LIU T S, RISIUS S . In-situ calibration for temperature-sensitive-paint heat-flux measurement on a finite base[J ] . International Journal of Heat and Mass Transfer, 2019 , 140 : 420 − 425 .
LIU T S, MONTEFORT J, SCHICK N, et al . Correction for effect of temperature-dependent diffusivity on temperature-sensitive-paint heat-flux measurement[J ] . International Journal of Heat and Mass Transfer, 2019 , 137 : 337 − 348 .
NAGAI H, OHMI S, ASAI K, et al . Effect of temperature-sensitive-paint thickness on global heat transfer measurement in hypersonic flow[J ] . Journal of T hermophysics and Heat Transfer, 2008 , 22 ( 3 ): 373 − 381 .
BOROVOY V, MOSHAROV V, NOEV A, et al . Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels[J ] . EUCASS Proceedings Series, 2012 , 3 : 15 − 24 .
WATKINS A N, BUCK G M, LEIGHTY B D, et al . Using pressure- and temperature-sensitive paint on the aftbody of a capsule entry vehicle[J ] . AIAA Journal, 2009 , 47 ( 4 ): 821 − 829 .
BERRIDGE D, CHOU A, WARD C, et al. Hypersonic boundary-layer transition experiments in a Mach-6 quiet tunnel[C]// 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virigina: AIAA, 2010.
KLEIN C, HENNE U. Combination of temperature sensitive paint and carbon nanotubes for transition detection[C]// 53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida. Reston, Virginia: AIAA, 2015.
GONZALES J, SUZUKI K, SAKAUE H . Temporally and sp atially resolved pressure and temperature maps in hypersonic flow[J ] . International Journal of Heat and Mass Transfer, 2020 , 156 : 119782 .
FEY U, ENGLER R H, EGAMI Y, et al. Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW)[C]// 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03, Gottingen, Germany. IEEE, 2004: 77-88.
EGAMI Y, FEY U, KLEIN C, et al . Development of new two-component temperature-sensitive paint (TSP) for cryogenic testing[J ] . Measurement Science and Technology, 2012 , 23 ( 11 ): 115301 .
LEBON M T, HAMMER C F, KIM J . Gravity effects on subcooled flow boiling heat transfer[J ] . International Journal of Heat and Mass Transfer, 2019 , 128 : 700 − 714 .
MATSUDA Y, KAWANAMI O, ORIMO R, et al . Simultaneous measurement of gas-liquid interface motion and temperature distribution on heated surface using temperature-sensitive paint[J ] . International Journal of Heat and Mass Transfer, 2020 , 153 : 119567 .
ZHU Y D, CHEN X, WU J Z, et al . Aerodynamic heating in transitional hypersonic boundary layers: role of second-mode instability[J ] . Physics of Fluids, 2018 , 30 ( 1 ): 011701 .
ZHU Y D, LEE C B, CHEN X, et al . Newly identified principle for aerodynamic heating in hypersonic flows[J ] . Journal of Fluid Mechanics, 2018 , 855 : 152 − 180 .
ZHANG K L, ZHOU J S, KONG R Z, et al . Development of TSP technique in shock tunnel of CARDC[J ] . Acta Aerodynamica Sinica, 2016 , 34 ( 6 ): 738 − 743 (in Chinese).
PENG D, JIAO L R, SUN Z J, et al . Simultaneous PSP and TSP measurements of transient flow in a long-duration hypersonic tunnel[J ] . Experiments in Fluids, 2016 , 57 ( 12 ): 188 .
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 (in Chinese).
LIU X, PENG D, LIU Y Z . Methods and applications of heat flux measurement using TSP[J ] . Physics of Gases, 2020 , 5 ( 5 ): 1 − 12 (in Chinese).
HUO J J, YI S H, NIU H B, et al . Experimental study of flow on the leeward side of a cone at a high angle of attack based on temperature sensitive paint[J ] . Physics of Gases, 2022 , 7 ( 4 ): 67 − 76 (in Chinese).
YUAN C K, MENG F Z, LIU X, et al . Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation[J ] . Acta Mechanica Sinica, 2023 , 39 ( 8 ): 322474 .
COOK W J, FELDERMAN E J . Reduction of data from thin-film heat-transfer gages - A concise numerical technique[J ] . AIAA Journal, 1966 , 4 ( 3 ): 561 − 562 .
EWING J, GIFFORD A, HUBBLE D, et al . A direct-measurement thin-film heat flux sensor array [J ] . Measurement Science and Technology, 2010 , 21 ( 10 ): 105201 .
KAMEYA T, MATSUDA Y, EGAMI Y, et al . Dual luminescent arrays sensor fabricated by inkjet-printing of pressure- and temperature-sensitive paints[J ] . Sensors and Actuators B:Chemical, 2014 , 190 : 70 − 77 .
EGAMI Y, UEYAMA J, FURUKAWA S, et al . Development of fast response bi-luminophore pressure-sensitive paint by means of an inkjet printing technique[J ] . Measurement Science and Technology, 2015 , 26 ( 6 ): 064004 .
PENG D, LIU Y Z . A grid-pattern PSP/TSP system for simultaneous pressure and temperature measurements[J ] . Sensors and Actuators B:Chemical, 2016 , 222 : 141 − 150 .
BAQERSAD J, POOZESH P, NIEZRECKI C, et al . Photogrammetry and optical methods in structural dynamics: A review[J ] . Mechanical Systems and Signal Processing, 2017 , 86 : 17 − 34 .
DONG Z, LIANG L, ZHANG W G, et al . Simultaneous pressure and deformation field measurement on helicopter rotor blades using a grid-pattern pressure-sensitive paint system[J ] . Measurement, 2020 , 152 : 107359 .
ZHU Y D, GU D W, ZHU W K, et al . Dilatational-wave-induced aerodynamic cooling in transitional hypersonic boundary layers[J ] . Journal of Fluid Mechanics, 2021 , 911 : A36 .
SCHNEIDER S P . Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: the role of quiet tunnels[J ] . Progress in Aerospace Sciences, 2015 , 72 : 17 − 29 .
GONZALEZ R C. Digital image processing[M]. Pearson Education India, 2009.
WESTERWEEL J, DABIRI D, GHARIB M . The effect of a discrete window offset on the accuracy of cross-correlation analysis of digital PIV recordings[J ] . Experiments in Fluids, 1997 , 23 ( 1 ): 20 − 28 .
WILLERT C . Stereoscopic digital particle image velocimetry for application in wind tunnel flows[J ] . Measurement Science and Technology, 1997 , 8 ( 12 ): 1465 − 1479 .
SCARANO F, RIETHMULLER M L . Advances in iterative multigrid PIV image processing[J ] . Experiments in Fluids, 2000 , 29 ( 1 ): S051 − S060 .
THIELICKE W, STAMHUIS E J. PIVlab–towards user-friendly, affordable and accurate digital particle image velocimetry in MATLAB[J]. Journal of Open Research Software, 2014, 2(1).
COOK W J . Determination of heat-transfer rates from transient surface temperature measurements[J ] . AIAA Journal, 1970 , 8 ( 7 ): 1366 − 1368 .
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