[1] Liu T, Sullivan J P. Pressure and temperature sensitive paints[M]. Berlin: Springer, 2005.

[2] Bencic T J. Rotating pressure and temperature measurements on scale model fans using luminescent paints[C]//Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 1998.

[3] Watkins A N, Goad W K, Obara C J, et al. Flow visualization at cryogenic conditions using a modified pressure-sensitive paint approach[C]//Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2005.

[4] Erickson G E, Gonzalez H A. Pressure-sensitive paint investigation of double delta wing vortex flow manipulation[C]//Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2005.

[5] Mérienne M C, Le Sant Y. Reliable PSP application and data processing at low speed flow conditions[C]//Proceedings of the 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston: AIAA, 2006.

[6] Shimbo Y, Noguchi M, Makino Y. Blowdown tunnel application of pressure sensitive paint[C]//Proceedings of the 17th AIAA Applied Aerodynamics Conference. Reston: AIAA, 1999.

[7] Kojima T, Nagai H, Asai K, et al. Application of lifetime PSP imaging method to a cryogenic wind tunnel[C]//Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2006.

[8] Merienne M C, Molton P, Bur R. Image measurement of oscillating shock wave by anodized-aluminum PSP[C]//Proceedings of the 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston: AIAA, 2010.

[9] Li G S, Zhou Q, Liu X, et al. Experimental research of pressure sensitive paint performance and calibration technique[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2): 227-234. (in Chinese) 李国帅, 周强, 刘祥, 等. 压力敏感涂料特性及其校准技术实验研究[J]. 航空学报, 2013, 34(2): 227-234.

[10] Zhang Y C, Chen L S, Yan L, et al. Investigation and application of pressure sensitive paint technique in wind tunnel test[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(1): 74-78. (in Chinese) 张永存, 陈柳生, 阎莉, 等. 压敏涂料技术在风洞中的应用研究[J]. 实验流体力学, 2010, 24(1): 74-78.

[11] Gao L M, Gao J, Wang H, et al. Application of PSP technique to pressure measurement on cascade surface[J]. Journal of Engineering Thermophysics, 2011, 32(3): 411-414. (in Chinese) 高丽敏, 高杰, 王欢, 等. PSP测量技术在叶栅表面压力测量中的应用[J]. 工程热物理学报, 2011, 32(3): 411-414.

[12] 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) 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.

[13] Borovoy V, Bykov A, Mosharov V, et al. Pressure sensitive paint application in shock wind tunnel[C]//Instrumentation in Aerospace Simulation Facilities. Wright-Patterson AFB: IEEE, 1995.

[14] Carroll B F, Abbitt J D, Lukas E W M, et al. Pressure sensitive paint response to a step pressure change[C]//Proceedings of the 33rd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1995.

[15] Hirose Y, Nagai H, Asai K. Unsteady flow measurements of a slender delta wing in wing rock motion[C]//Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2007.

[16] Nakakita K. Unsteady pressure distribution measurement around 2d-cylinders using pressure-sensitive paint[C]//Proceedings of the 25th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2007.

[17] Yarusevych S, Kawall J G, Sullivan J P. Unsteady separated flow characterization on airfoils using time-resolved surface pressure measurements[J]. AIAA Journal, 2008, 46(2): 508-516.

[18] Nakakita K. Scanning unsteady PSP technique for high-frequency and small-pressure fluctuation in low-speed[C]//Proceedings of the 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston: AIAA, 2010.

[19] Schairer E T. Optimum thickness of pressure-sensitive paint for unsteady measurements[J]. AIAA Journal, 2002, 40(11): 2312-2318.

[20] Asai K, Kanda H, Cunningham C T, et al. Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating[C]//Instrumentation in Aerospace Simulation Facilities. Pacific Grove: IEEE, 1997.

[21] Asai K, Amao Y, Iijima Y, et al. Novel pressure-sensitive paint for cryogenic and unsteady wind-tunnel testing[J]. Journal of Thermophysics and Heat Transfer, 2002, 16(1): 109-115.

[22] Erausquin R, Cunningham C T, Sullivan J P, et al. Cryogenic pressure sensitive fluorescent paint systems[C]//Proceedings of the 36th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1998.

[23] Lin Y, Chen L S, Shi Y, et al. Rapid-response atmospheric oxygen sensor based on adsorption of dimethyl (octyl) (4-(pyren-4-yl) butoxy) silane[J]. Sensor Letters, 2007, 5(3-4): 3-4.

[24] Chen L S, Zhou Q, Jin X G, et al. Pressure-sensitive paint and its measuring technique[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(12): 2435-2448.(in Chinese) 陈柳生, 周强, 金熹高, 等. 压力敏感涂料及其测量技术[J]. 航空学报, 2009, 30(12): 2435-2448.

[25] Qin S, Chen L S, Shi Y, et al. Fabrication of microporous thin film from polyelectrollyte multilayer films[J]. Chemical Journal of Chinese Universities, 2005, 26(6): 1183-1185.(in Chinese) 秦胜, 陈柳生, 史燚, 等. 由聚电解质自组装多层膜制备微孔薄膜[J]. 高等学校化学学报, 2005, 26(6): 1183-1185.

[26] Gao J. Image 3D reconstruction and research of PSP measurement technique[D]. Xi’an: School of Power and Energy, Northwestern Polytechnical University, 2012. (in Chinese) 高杰. 图像三维重构及PSP测量技术研究[D]. 西安: 西北工业大学动力与能源学院, 2012.

[27] Sakaue H, Sullivan J P. Time response of anodized aluminum pressure-sensitive paint[J]. AIAA Journal, 2001, 39(10): 1944-1949.

[28] Mosharov V, Orlov A, Radchenko V, et al. Luminescent pressure sensors for aerospace research: diffusion-controlled characteristics[C]//Proceedings of the 2nd European Conference on Optical Chemical Sensors and Biosensors. Firenze: Center of Chemical Sensors and Biosensors, 1994.

[29] Hubner J P, Carroll B F, Schanze K S, et al. Techniques for using pressure-sensitive paint in shock tube facilities[C]//International Congress on Instrumentation in Aerospace Simulation Facilities, 1997.

[30] Carroll B E, Abbitt J D, Likas E W, et al. Step response of pressure-sensitive paints [J]. AIAA Journal, 1996, 34(3): 521-526.

[31] Sakaue H, Gregory J W, Sullivan J P, et al. Porous pressure sensitive paint for unsteady flow fields[C]//Proceedings of the 39th Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2001.

[32] Sakaue H, Sullivan J P. Fast response time characteristics of anodized aluminum pressure sensitive paint[C]//Proceedings of the 38th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2000.

[33] Schairer E T. Optimum thickness of pressure-sensitive paint for unsteady measurements[J]. AIAA Journal, 2002, 40(11): 2312-2318.

[34] Scroggin A M. Processing and optimization of doped polymer/ceramic composite films for luminescence-based pressure and temperature measurement in aerodynamic applications[D]. West Lafayette: School of Material Science and Engineering, Purdue University, 1999.

[35] Baron A E, Danielson J D S, Gouterman M, et al. Submillisecond response times of oxygen-quenched luminescent coatings[J]. Review of Scientific Instruments, 1993, 64(12): 3394-3402.

[36] Sakamura Y, Suzuki T, Matsumoto M, et al. Optical measurements of high-frequency pressure fluctuations using a pressure-sensitive paint and cassegrain optics[J]. Measurement Science and Technology, 2002, 13(10): 1591.

[37] Sakamura Y, Matsumoto M, Suzuki T. High frame-rate imaging of surface pressure distribution using a porous pressure-sensitive paint[J]. Measurement Science and Technology, 2005, 16(3): 759.

[38] Mérienne M C, Le Sant Y, Ancelle J, et al. Unsteady pressure measurement instrumentation using anodized-aluminium PSP applied in a transonic wind tunnel[J]. Measurement Science and Technology, 2004, 15(12): 2349.

[39] Sakaue H, Tabei T, Kameda M. Hydrophobic monolayer coating on anodized aluminum pressure-sensitive paint[J]. Sensors and Actuators B: Chemical, 2006, 119(2): 504-511.

[40] Sakaue H, Mitsuo K, Iijima Y, et al. Application of luminophore pendant pressure sensitive paint to fluid dynamic measurements[C]//Proceedings of the 12th International Symposium on Flow Visualization. Gottingen: ISFV, 2006.

[41] Sakaue H, Sullivan J P, Asai K, et al. Anodized aluminum pressure sensitive paint in a cryogenic wind tunnel[C]//Proceedings of the International Instrumentation Symposium. Orland Park: American Technical Publishers LTD, 1999.

[42] Scroggin A M, Slamovich E B, Crafton J W, et al. Porous polymer/ceramic composites for luminescence-based temperature and pressure measurement[C]//Proceedings of the Materials Research Society Symposium, 1999, 560: 347-352.

[43] Gregory J W, Sakaue H, Sullivan J P. Unsteady pressure measurements in turbomachinery using porous pressure sensitive paintt[C]//Proceedings of the 40th Aerospace Sciences Meeting & Exhibit. Reston: AIAA, 2002.

[44] Ponomarev S, Gouterman M. Fast responding pressure sensitive paints based on high concentration of hard particles in polymer[C]//Proceedings of the 6th Annual Pressure-sensitive Paint Workshop. Seattle: The Boeing Co., 1998.

[45] Kameda M, Tabei T, Nakakita K, et al. Image measurements of unsteady pressure fluctuation by a pressure-sensitive coating on porous anodized aluminium[J]. Measurement Science and Technology, 2005, 16(12): 2517.

[46] Fang S, Long S R, Disotell K J, et al. Comparison of unsteady pressure-sensitive paint measurement techniques[J]. AIAA Journal, 2012, 50(1): 109-122.

[47] Mitsuo K, Egami Y, Suzuki H, et al. Development of lifetime imaging system for pressure-sensitive paint[C]//Proceedings of the 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston: AIAA, 2002.

[48] Asai K, Yorita D. Unsteady PSP measurement in low speed flow—overview of recent advancement at Tohoku University[C]//Proceedings of the 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2011.

[49] Gregory J W, Sullivan J P, Wanis S S, et al. Pressure-sensitive paint as a distributed optical microphone array[J]. The Journal of the Acoustical Society of America, 2006, 119(1): 251-261.

[50] Yorita D, Nagai H, Asai K, et al. Unsteady PSP technique for measuring naturally-disturbed periodic phenomena[C]//Proceedings of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2010.

[51] Gregory J W, Sullivan J P, Raman G, et al. Characterization of the microfluidic oscillator[J]. AIAA Journal, 2007, 45(3): 568-576.

[52] Hirofumi O, Tomoko I, Kozo F, et al. PSP measurements in the large-scale transonic wind tunnel and associated image data processing[C]//Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2005.

[53] Zare-Behtash H, Gongora N, Lada C, et al. Application of pressure sensitive paint measurements to complex flows[C]//Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2008.

[54] Lakshminarayana B. Techniques for aerodynamic and turbulence measurements in turbomachinery rotors[J]. Journal of Engineering for Power, 1981, 103(2): 374-392.

[55] Whale J, Papadopoulos K H, Anderson C G, et al. A study of the near wake structure of a wind turbine comparing measurements from laboratory and full-scale experiments[J]. Solar Energy, 1996, 56(6): 621-633.

[56] Gao L M, Xi G, Zhou L, et al. Experimental and computational investigation of flows in a vaned diffuser under stage environment[J]. Chinese Journal of Theoretical and Applied Mechanics, 2005, 37(1): 110-119. (in Chinese) 高丽敏, 席光, 周莉, 等. 级环境下叶片扩压器流场的实验与数值研究[J]. 力学学报, 2005, 37(1): 110-119.

[57] Singh M,Naughton J W, Yamashita T, et al. Surface pressure and flow field behind an oscillating fence submerged in turbulent boundary layer[J]. Experiments in Fluids, 2011, 50(3): 701-714.

[58] Lu T, Shi Y, Wang H. High-speed data acquisition circuit design of a digital signal analyzer[C]//Proceedings of 2005 International Conference on Communications, Circuits and Systems. Hong Kong: IEEE, 2005.

[59] Song Y X. Study on some key technologies of high-speed image acquisition processing system[D]. Harbin: School of Electrical Engineering and Automation, Harbin Institute of Technology, 2010. (in Chinese) 宋燕星. 高速图像采集处理系统中若干关键技术的研究[D]. 哈尔滨: 哈尔滨工业大学电气工程学院, 2010.

[60] Nakakita K, Arizono H. Visualization of unsteady pressure behavior of transonic flutter using pressure-sensitive paint measurement[C]//Proceedings of the 27th Applied Aerodynamics Conference. Reston: AIAA, 2009.

[61] Nakakita K, Kurita M, Mitsuo K, et al. Practical pressure-sensitive paint measurement system for industrial wind tunnels at JAXA[J]. Measurement Science and Technology, 2006, 17(2): 359.

[62] Miyamoto K, Miyazaki T, Sakaue H. Development of motion-cancelled PSP system and its application to a helicopter blade[C]//Proceedings of the 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston: AIAA, 2010.

[63] Konrath R, Klein C, Engler R H, et al. Analysis of PSP results obtained for the VFE-2 65 delta wing configuration at sub-and transonic speeds[C]//Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2006.

[64] Klein C, Henne U, Sachs W E, et al. Application of pressure-sensitive paint for determination of dynamic surface pressures on a rotating 65° delta wing and an oscillating 2D profile in transonic flow[C]//Proceedings of the 22nd International Congress on Instrumentation in Aerospace Simulation Facilities. Pacific Grove: IEEE, 2007: 1-7.