正弦波型高频动态压力光学校准系统及其应用

doi:10.7527/S1000-6893.2020.23667

Abstract

Abstract: Dynamic pressure is a key aerodynamic parameter on pneumatic model surfaces. An optical technique using Pressure-Sensitive Paint (PSP) provides an advantage in obtaining full-field and low aerodynamic interference images during measurement of dynamic pressure on pneumatic model surfaces, while the dynamic response characteristic of the optical pressure sensitive paint is critical to dynamic pressure measurement. Based on the principle of acoustic standing wave tubes, a high frequency dynamic pressure optical calibration system with sinusoidal waves is designed and established independently, including a calibration chamber based on the standing wave tube, a sound source, a laser, a high frequency dynamic pressure transducer, a photo multiplier tube, and a system for measurement and control. The test results of the dynamic pressure optical calibration system and a new kind of fast pressure sensitive paint indicate that the shortest response time of the dynamic pressure calibration system, set up independently, is 12.5 μs, while the largest sinusoidal dynamic pressure amplitude can reach up to 4.37 kPa, with the valid dynamic frequency varying from 0.4 to 20.0 kHz (50 μs~2.5 ms), and the uncertainty less than 0.004 9%; reasonable light layout of the calibration system guarantees the calibration of dynamic characteristics for fast pressure sensitive paint, and the paint measured can be utilized in pressure measurement of unsteady flow fields with a dynamic frequency below 9.1 kHz (response time of 109.9 μs).

Key words: optical pressure sensitive paint, acoustic standing wave tubes, sinusoidal waves, high frequency dynamic pressure, optical calibration system

CLC Number:

V231.3

GAO Limin, JIANG Heng, GE Ning, YANG Guanhua, ZHAO Chongxiang. A high frequency dynamic pressure optical calibration system based on sinusoidal wave and its application[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(10): 123667-123667.

References

[1] LIU T, SULLIVAN J P. 压力敏感涂料与温度敏感涂料[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).
[2] 高丽敏, 吴亚楠, 胡小全, 等. 基于光强的快速响应PSP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):607-632(in Chinese).
[3] SUGIMOTO T, KITASHIMA S, NUMATA D, et al. Characterization of frequency response of pressure-sensitive paints[J].AIAA Journal, 2017, 55(4):1460-1464.
[4] 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.
[5] 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.
[6] PENG D, GU F, LI Y Z, et al. A novel sprayable fast-responding pressure-sensitive paint based on mesoporous silicone dioxide particles[J].Sensors & Actuators:A Physical, 2018, 279:390-398.
[7] PENG D, WANG S F, LIU Y Z. Fast PSP measurements of wall-pressure fluctuation in low-speed flows:Improvements using proper orthogonal decomposition[J].Experiments in Fluids, 2016, 57(4):1-17.
[8] PENG D, LIU Y. Fast pressure-sensitive paint for understanding complex flows:From regular to harsh environments[J].Experiments in Fluids, 2020, 61(1):8.
[9] BORBYE J. Experimental investigation of frequency response of unsteady pressure sensitive paint and application for an oscillating airfoil[D]. Lyngby:Technical University of Denmark, 2008:20-25.
[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] ANSHUMAN P, JAMES G. Step response characteristics of polymer/ceramic, pressure-sensitive paint[J].Sensors, 2015, 15(9):22304-22324.
[12] JIAO L, PENG D, LIU Y, et al. Dynamic response of polymer ceramic pressure-sensitive paint:Improved model considering thickness effect[J].AIAA Journal, 2018, 56(7):2903-2906.
[13] 丰雷. 影响激波管动态压力校准精度的关键问题研究[D]. 太原:中北大学, 2016:17-30. FENG L. Research of key problems affecting dynamic pressure calibration precision of shock tube[D]. Taiyuan:North University of China, 2016:17-30(in Chinese).
[14] 高丽敏, 姜衡, 郑天龙, 等. 正弦式光学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).
[15] TAMAO S, SAKIKO K, DAIJU N, et al. Characterization of frequency response of pressure-sensitive paints[J].AIAA Journal, 2012, 55(4):1460-1464.
[16] PANDEY A, GREGORY J W. Frequency-response characteristics of polymer/ceramic pressure-sensitive paint[J].AIAA Journal, 2016, 54(1):174-185.
[17] 杜功焕, 朱哲民, 龚秀芬. 声学基础[M]. 南京:南京大学出版社, 2012:226-244. DU G H, ZHU Z M, GONG X F. Fundamentals of acoustics[M]. Nanjing:Nanjing University Press, 2012:226-244(in Chinese).
[18] 熊健, 李国帅, 周强, 等. 2.4 m跨声速风洞压敏漆测量系统研制与应用研究[J].实验流体力学, 2016, 30(3):76-84. XIONG J, LI G S, ZHOU Q, et al. Development and application of pressure sensitive paint system in 2.4 m transonic wind tunnel[J].Journal of Experiments in Fluid Mechanics, 2016, 30(3):76-84(in Chinese).
[19] 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.
[20] 闵琦, 刘克. 锥形变截面驻波管及其极高纯净驻波场的实验研究[J].声学学报, 2011, 36(6):645-651. MIN Q, LIU K. Experimental study on tapered variable section of standing-wave tube and its extremely high purity standing-wave fields[J].Journal of Acoustics, 2011, 36(6):645-651(in Chinese).
[21] FUNDERBURK M L, NARAYANASWAMY V. Spectral signal quality of fast pressure sensitive paint measurements in turbulent shock-wave/boundary layer interactions[J].Experiments in Fluids, 2019, 60(10):154.
[22] WEN X, LIU Y, LI Z, et al. Data mining of a clean signal from highly noisy data based on compressed data fusion:A fast-responding pressure-sensitive paint application[J].Physics of Fluids, 2018, 30(9):097103.
[23] 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).

A high frequency dynamic pressure optical calibration system based on sinusoidal wave and its application

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	. Numerical Study of Elliptic Flow Noise Problems by an Improved Ghost-cell Immersed Boundary Method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[2]	. Unsteady simulation of stall process in a transonic compressor with total temperature distortion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[3]	. Experimental data driven cascade flow field prediction based on data assimilation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[4]	Qiu-Lin LI Peng SUN Jingwei SHi WANG Zhan-Xue. Investigation on Influence Mechanism of Aspect Ratio on Fluid-Structure Interaction Characteristic of Serpentine Nozzle [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[5]	. Flow Measurement and Analysis of a Turbine Blade With Multiple Cooling Structures Based on Magnetic Resonance Velocimetry [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[6]	WEI Yongbin, DUAN Zhuoyi, GUO Zhaodian, YANG Chengfeng. Parameterization investigation method for nacelle aerodynamic performance [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526742-526742.
[7]	DU Jianjian, PAN Xiande, LIU Tianyi. Indirect measurement method for axial load of aero-engine angular contact ball bearing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 625457-625457.
[8]	AN Liping, WANG Hao, WANG Yangang, ZHU Zihuan. Wet compression performance and flow characteristics of transonic compressor [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 126024-126024.
[9]	. Design of inward turning inlet with controlled Mach number under non-uniform inflow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[10]	. Experimental study on cut-off frequency of a certain type of domestic fast response PSP [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[11]	. Investigation of the Flow Mechanism of Swept and Bowed Blades with Considera-tion of the Circumferential Fluctuation Source Term before Blade Leading Edge [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[12]	YAN Qun, XUE Dongwen, GAO Xiang, YANG Jiafeng, HUANG Wenchao. Acoustic performance experimental technology of aircraft nacelle acoustic liner [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526810-526810.
[13]	. Statistical Study on the Geometric Uncertainties of Casting Blades in a Low-Pressure Turbine [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.
[14]	ZHAO Le, WANG Wei, ZHANG Lefu, WANG Weichao, LU Jinling, CHU Wuli. Coupling method for stability improvement for transonic compressor at variable speed [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 124942-124942.
[15]	. Experimental study on composite rim seal with deep cavity in the static disc and modified platform [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0, (): 0-0.