基于寿命法的压力敏感涂料静/动态特性实验

doi:10.7527/S1000-6893.2020.24120

Abstract

Abstract: The pressure sensitive paint metrical technique has unique advantages in surface pressure measurements of internal and external flow fields. The study of spectral characteristics and "transducer" characteristics of paints is of vital significance for impact analysis of uncontrollable factors such as differences of surroundings in spraying and curing and applicability verification of specific tests for proposed paint formulas. Therefore, taking a phosphorescent pressure sensitive paint under research as the object, we conduct an experimental research on the variation law of luminescent lifetime with pressure and temperature based on a self-developed static calibration system. Fitting analysis of the measured results shows that the applicable temperature of the paint is between 30 ℃ and 60 ℃, which can be modified by temperature sensitivity. In addition, based on the self-developed high frequency dynamic pressure optical calibration system, the law of the pressure sensitive paint lifetime peak-to-peak values with different pressure pulsation frequencies is studied experimentally. Analysis ascertains that the cut-off frequency upper limit of the paint based on the luminescent lifetime is 0.94 kHz. The feasibility and effectiveness of the combination method for static and dynamic calibration of paint characteristics are further verified by experimental studies, providing important technical support for the research and development of pressure sensitive paint formulations and applications.

Key words: pressure sensitive paints, pressure measurements, lifetime method, static characteristics, dynamic characteristics

CLC Number:

V231.3

GAO Limin, JIANG Heng, GE Ning, YANG Guanhua, CHEN Shun. Experiment on static/dynamic characteristics of fast-response pressure sensitive paint based on lifetime method[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124120-124120.

References

[1] 郑文涛, 蒋永松, 赵航, 等. 风扇出口导向叶片低噪声设计Ⅱ:数值验证[J]. 航空学报, 2019, 40(10):122956. ZHENG W T, JIANG Y S, ZHAO H, et al. Low noised design fan outlet guide vane, part Ⅱ:Numerical verifications[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(10):122956(in Chinese).
[2] MEARS L, ARORA N, ALVI F. Flowfield response to controlled perturbations in swept shock/boundary-layer interaction using unsteady PSP:AIAA-2019-0094[R]. Reston:AIAA, 2019.
[3] 高丽敏, 吴亚楠, 胡小全, 等. 基于光强的快速响应动态测量技术及其应用[J]. 航空学报, 2014, 35(3):607-623. GAO L M, WU Y N, HU X Q, et al. Intensity-based fast response PSP technique and its applications[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3):607-623(in Chinese).
[4] WONG O D, WATKINS A N, INGRAM J L. Pressure sensitive paint measurements on 15% scale rotor blades in hover:AIAA-2005-5008[R]. Reston:AIAA, 2005.
[5] PUKLIN E, CARLSON B, GOUIN S, et al. Ideal pressure sensitive paint:PtTFPP in FIB polymer[C]//Proceedings of the Sixth Annual Pressure Sensitive Paint Workshop. Seattle:Boeing Company, 1998:1-22.
[6] JI H, SHEN Y, HUBNER J P, et al. Temperature independent pressure-sensitive paint based on a bichromophoric luminophore[J]. Applied Spectroscopy, 2000, 54(6):856-863.
[7] 高丽敏,王欢,刘波, 等.测量系统特性对压敏涂料校准影响的实验研究[J]. 航空学报, 2010, 31(1):76-81. GAO L M, WANG H, LIU B, et al. Experimental of study influence of measurement system characteristics on pressure sensitive paint calibration[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(1):76-81(in Chinese).
[8] 刘波,周强,靳军,等. 压力敏感涂料技术及其应用[J]. 航空动力学报, 2006, 21(2):225-233. LIU B, ZHOU Q, JIN J, et al. Applications of pressure sensitive paint technique[J]. Journal of Aerospace Power, 2006, 21(2):225-233(in Chinese).
[9] PENG D, LIU Y Z. A grid-pattern PSP/TSP system for simultaneous pressure and temperature measurements[J]. Sensors & Actuators B:Chemical, 2016, 222:141-150.
[10] LI R Y, GAO L M, ZHENG T L, et al. Experimental investigation on static/dynamic characteristics of a fast-response pressure sensitive paint[J]. Chinese Journal of Aeronautics, 2018, 31(6):1198-1205.
[11] PENG D, LIU Y Z. Fast pressure-sensitive paint for understanding complex flows:From regular to harsh environments[J]. Experiments in Fluids, 2020, 61:8.
[12] DISOTELL K J, PENG D, JULIANO T J, et al. Single-shot temperature-and pressure-sensitive paint measurement on an unsteady helicopter blade[J]. Experiments in Fluids, 2014, 55:1671.
[13] WATKINS A N, LEIGHTY B D, LIPFORD W E, et al. Measuring surface pressures on rotor blades using pressure-sensitive paint[J]. AIAA Journal, 2016, 54(1):206-215.
[14] PENG D, JIAO L, YU Y, et al. Single-shot lifetime-based PSP and TSP measurements on turbocharger compressor blades[J]. Experiments in Fluids, 2017, 58:127.
[15] RUYTEN W. Assimilation of physical chemistry models for lifetime analysis of pressure-sensitive paint[J]. AIAA Journal, 2005, 43(3):465-471.
[16] YORITA D, HENNE U, KLEIN C. Improvement of lifetime-based PSP technique for industrial wind tunnel test:AIAA-2017-0703[R]. Reston:AIAA, 2017.
[17] 高丽敏,姜衡,郑天龙,等. 正弦式压力敏感涂料动态压力校准舱:CN109269720A[P]. 2019-01-25. GAO L M, JIANG H, ZHENG T L, et al. Sinusoidal dynamic pressure calibration chamber for optical pressure sensitive paints:CN109269720A[P]. 2019-01-25(in Chinese).
[18] 高丽敏,姜衡,葛宁,等. 正弦波型高频动态压力光学校准系统及其应用[J]. 航空学报, 2020, 41(10):123667. GAO L M, JIANG H, GE N, et al. Research and application of a high frequency dynamic pressure optical calibration system based on sinusoidal wave[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10):123667(in Chinese).
[19] LIU T, SULLIVAN J P. 压力敏感涂料与温度敏感压力敏感涂料[M]. 周强,陈柳生,马护生,等, 译. 北京:国防工业出版社, 2012:12-19. LIU T, SULLIVAN J P. Pressure and temperature sensitive paints[M]. ZHOU Q, CHEN L S, MA H S, et al., translated. Beijing:National Defense Industry Press, 2012:12-19(in Chinese).
[20] PRADEEP K. Development of a single-shot lifetime PSP measurement technique for rotating surfaces[D]. Columbus:The Ohio State University, 2010.
[21] 曹光跃, 徐文璞.传感器原理及应用[M]. 北京:化学工业出版社, 2010:8-10. CAO G Y, XU W P. Sensor principles and applications[M]. Beijing:Chemical Industry Press, 2010:8-10(in Chinese).
[22] JIN B Q, LI Y Q, SHI Y, et al. Effect of polymer matrix on the photophysical behaviors of pressure sensitive films[J]. Polymer, 2017, 116(5):466-471.
[23] 杨旭, 孙宏凯, 许佳胜. 浅析Nyquist-Shannon采样定理[J].中国新通信,2020,22(2):168. YANG X, SUN H K, XU J S. A brief analysis of Nyquist-Shannon sampling theorem[J]. China New Telecommunications, 2020, 22(2):168(in Chinese).
[24] 姚萍萍, 孙亮, 许孙龙, 等. 科学级CCD制冷系统设计及其温度特性分析[J].光学学报, 2020, 40(17):1704001. YAO P P, SUN L, XU S L, et al. Design of scientific CCD refrigeration system and analysis of its temperature characteristics[J]. Acta Optica Sinica, 2020, 40(17):1704001(in Chinese).

Experiment on static/dynamic characteristics of fast-response pressure sensitive paint based on lifetime method

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