Yu Jingbo, Xiang Xingju, Xiong Hongliang, et al. Measurements and applications of fast response pressure sensitive paint[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(3): 17-32. doi: 10.11729/syltlx20180007
Citation: Yu Jingbo, Xiang Xingju, Xiong Hongliang, et al. Measurements and applications of fast response pressure sensitive paint[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(3): 17-32. doi: 10.11729/syltlx20180007

Measurements and applications of fast response pressure sensitive paint

doi: 10.11729/syltlx20180007
  • Received Date: 2018-01-22
  • Rev Recd Date: 2018-04-23
  • Publish Date: 2018-06-25
  • The fast response pressure sensitive paint measurement technique has been developed quickly in recent years. A general review of this technique based on detailed investigation is presented. The characteristic, principle and dynamic response mechanism are described. Three kinds of porous structure fast response pressure sensitive paint are introduced, including TLC-PSP, AA-PSP and PC-PSP. Several dynamic calibration devices are introduced, including the shock wave tube, fast response solenoid valve, loudspeaker, jet oscillator and pulse jet. Different measurement methods are introduced including the point measurement, phase averaging, high speed acquiring, motion-capture measurement, life time method, and PSP microspheres method. Different application cases around the world are introduced, which manifests the advantages of the fast response PSP technique on the unsteady flow measurement.
  • loading
  • [1]
    Liu T, Sullivan J P. Pressure and temperature sensitive paints[M]. Berlin:Springer, 2005.
    [2]
    陈柳生, 周强, 金喜高, 等.压力敏感涂料及其测试技术[J].航空学报, 2009, 30(12):2435-2448. doi: 10.3321/j.issn:1000-6893.2009.12.029

    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. doi: 10.3321/j.issn:1000-6893.2009.12.029
    [3]
    Gregory J W, Asai K, Kameda M, et al. A review of pressure-sensitive paint for high-speed and unsteady aerodynamics[J]. Proc IMechE G J Aerosp Eng, 2008, 222(2):249-90. doi: 10.1243/09544100JAERO243
    [4]
    Gregory J W, Sakaue H, Liu T, et al. Fast pressure-sensitive paint for flow and acoustic diagnostics[J]. Annu Rev Fluid Mech, 2014, 46(1):303-30. doi: 10.1146/annurev-fluid-010313-141304
    [5]
    Engler R H, Klein C, Merlo E, et al. 360 degree PSP measurements in transonic flow[C]. 19th International Congress on Instrumentation in Aerospace Simulation Facilities, Cleveland, Ohio, 2001. http://www.researchgate.net/publication/3920446_360_PSP_measurements_in_transonic_flow
    [6]
    Pervushin G E, Nevsky L B. Composition for indicating coatin[P]. Russian: USSR-SU 1065452, 1981.
    [7]
    Gouterman M, Callis J, Burns D, et al. Luminescence imaging for aerodynamic testing[C]. ONR/NASA Workshop on Quantitative Flow Visualization, Purdue University, West Lafayette, IN, USA, 1990.
    [8]
    Davies A G, Bedwell D, Dunleavy M, et al. Pressure sensitive paint measurements using a phosphorescence lifetime method[C]. Seventh International Symposium on Flow Visualization, Seattle, Washington, 1995.
    [9]
    Carroll B F, Abbitt J D, Lukas E W, et al. Step response of pressure sensitive paints[J]. AIAA Journal, 1996, 34(3):521-526. doi: 10.2514/3.13099
    [10]
    Winslow N A, Carroll B F, Kurdila A J. Model development and analysis of the dynamics of pressure-sensitive paints[J]. AIAA Journal, 2001, 39(4):660-666. doi: 10.2514/2.1359
    [11]
    Gregory J W, Sullivan J P. Effect of quenching kinetics on unsteady response of pressure-sensitive paint[J]. AIAA Journal, 2006, 44(3):634-645. doi: 10.2514/1.15124
    [12]
    Kameda M. Effect of luminescence lifetime on the frequency response of fast-response pressure-sensitive paints[J]. Trans Jpn Soc Mech Eng B, 2012, 78(795):1942-1950. doi: 10.1299/kikaib.78.1942
    [13]
    McMullen R M, Huynh D P, Gregory J W, et al. Dynamic calibrations for fast-response porous polymer/ceramic pressure-sensitive paint[C]. AIAA Ground Test, San Diego, CA, 2013. doi: 10.2514/6.2013-3123
    [14]
    Schairer E T. Optimum thickness of pressure-sensitive paint for unsteady measurements[J]. AIAA Journal, 2002, 40(11):2312-2318. doi: 10.2514/2.1568
    [15]
    Sakaue H, Sullivan J P. Time response of anodized aluminum pressure-sensitive paint[J]. AIAA Journal, 2001, 39(10):1944-1949. doi: 10.2514/2.1184
    [16]
    Liu T, Teduka N, Kameda M, et al. Diffusion timescale of porous pressure-sensitive paint[J]. AIAA Journal, 2001, 39(12):2400-2402. doi: 10.2514/2.1249
    [17]
    Kameda M, Tabei T, Nakakita K, et al. Image measurements of unsteady pressure fluctuation by a pressure-sensitive coating on porous anodized aluminum[J]. Meas Sci Technol, 2005, 16(12):2517-2574. doi: 10.1088/0957-0233/16/12/017
    [18]
    Gregory J W, Sullivan J P, Wanis S S, et al. Pressure-sensitive paint as a distributed optical microphone array[J]. Acoust Soc Am, 2006, 119(1):251-261. doi: 10.1121/1.2140935
    [19]
    Baron A E, Danielson J D S, Gouterman M, et al. Submillisecond response times of oxygen-quenched luminescent coatings[J]. Rev Sci Instrum, 1993, 64(12):3394-3402. doi: 10.1063/1.1144310
    [20]
    Sakaue H, Gregory J W, Sullivan J P, et al. Porous pressure-sensitive paint for characterizing unsteady flowfields[J]. AIAA Journal, 2002, 40(6):1094-1098. http://www.researchgate.net/publication/245425422_Porous_Pressure-Sensitive_Paint_for_Characterizing_Unsteady_Flowfields
    [21]
    Sakamura Y, Matsumoto M, Suzuki T. High frame-rate imaging of surface pressure distribution using a porous pressure-sensitive paint[J]. Meas Sci Technol, 2005, 16(3):759-765. doi: 10.1088/0957-0233/16/3/019
    [22]
    Gongora-Orozco N, Zare-Behtash H, Kontis K. Global unsteady pressure-sensitive paint measurements of a moving shock wave using thin-layer chromatography[J]. Measurement, 2010, 43(1):152-155. doi: 10.1016/j.measurement.2009.06.011
    [23]
    Sakaue H, Tabei T, Kameda M. Hydrophobic monolayer coating on anodized aluminum pressure sensitive paint[J]. Sens Actuators B, 2006, 119(2):504-511. doi: 10.1016/j.snb.2006.01.010
    [24]
    Zare-Behtash H, Yang L, Gongora-Orozco N, et al. Anodized aluminium pressure sensitive paint:effect of paint application technique[J]. Measurement, 2012, 45(7):1902-1905. doi: 10.1016/j.measurement.2012.03.015
    [25]
    Sakaue H, Morita K, Iijima Y, et al. Response time scales of anodized-aluminum pressure sensitive paints[J]. Sens Actuators A, 2013, 199(9):74-79. http://www.sciencedirect.com/science/article/pii/S0924424713002057
    [26]
    Ponomarev S, Gouterman M. Fast responding pressure sensitive paints based on high concentration of hard particles in polymer[C]. Proceedings of the Sixth Annual Pressure Sensitive Paint Workshop, The Boeing Company, Seattle, Washington, 1998.
    [27]
    Scroggin A M. Processing and optimization of luminescence based pressure and temperature sensors for aerodynamic applications[D]. Purdue University, 1999.
    [28]
    Gregory J W, Sullivan J P, Wanis S S, et al. Pressure-sensitive paint as a distributed optical microphone array[J]. Acoust Soc Am, 2006, 119(1):251-261. doi: 10.1121/1.2140935
    [29]
    Sakaue H, Kakisako T, Ishikawa H. Characterization and optimization of polymer-ceramic pressure sensitive paint by controlling polymer content[J]. Sensors, 2011, 11(7):6967-6977. doi: 10.3390/s110706967
    [30]
    Scroggin A M, Slamovich E B, Crafton J W, et al. Porous polymer/ceramic composites for luminescent-based temperature and pressure measurement[J]. Mater Res Soc Proc, 1999, 560:347-352. doi: 10.1557/PROC-560-347
    [31]
    Juliano T J, Disotell K J, Gregory J W, et al. Motion-deblurred, fast-response pressure sensitive paint on a rotor in forward flight[J]. Meas Sci Technol, 2012, 23(23):045303. http://www.ingentaconnect.com/content/iop/mst/2012/00000023/00000004/art045303
    [32]
    Sugimoto T, Kitashima S, Numata D, et al. Characterization of frequency response of pressure sensitive paints[R]. AIAA-2012-1185, 2012. http://www.researchgate.net/publication/269052314_Characterization_of_Frequency_Response_of_Pressure-Sensitive_Paints
    [33]
    Gregory J W, Sakaue H, Sullivan J P. Fluidic oscillator as a dynamic calibration tool[R]. AIAA-2002-2701, 2002. http://www.researchgate.net/publication/268559847_Fluidic_Oscillator_as_a_Dynamic_Calibration_Tool?ev=auth_pub
    [34]
    Kameda M, Seki H, Makoshi T, et al. A fast-response pressure sensor based on a dye-adsorbed silica nanoparticle film[J]. Sens Actuators B, 2012, 171-172(9):343-349. http://www.sciencedirect.com/science/article/pii/S0925400512004091/pdf?md5=4e1c449e27cbdbb762e49b7b9f369275&pid=1-s2.0-S0925400512004091-main.pdf&_valck=1
    [35]
    Asai K, Amao Y, Iijima Y, et al. Novel pressure-sensitive paint for cryogenic and unsteady wind-tunnel testing[J]. Thermophys Heat Transf, 2002, 16(1):109-115. doi: 10.2514/2.6658
    [36]
    Asai K, Nakakita K, Kameda M, et al. Recent topics in fast-responding pressure-sensitive paint technology at National Aerospace Laboratory[C]. Proc 19th Int Congr Instrum Aerosp Simul Facil, Piscataway, 2001.
    [37]
    Amao Y, Okura I, Shinohara H, et al. An optical sensing material for trace analysis of oxygen:metalloporphyrin dispersed in poly(1-trimethylsilyl-1-propyne) film[J]. Polym Journal, 2002, 34(34):411-417. http://www.nature.com/pj/journal/v34/n6/abs/pj200263a.html
    [38]
    Kameda M, Tezuka N, Hangai T, Asai K, et al. Adsorptive pressure-sensitive coatings on porous anodized aluminum[J]. Meas Sci Technol, 2004, 15(3):489-500. doi: 10.1088/0957-0233/15/3/001
    [39]
    Pastuhoff M, Tillmark N, Alfredsson P H. 2010. Dynamic calibration of polymer/ceramic pressure sensitive paint using a shock tube[C]. Proc 7th Int Conf Flow Dyn, Sendai, 2010.
    [40]
    Fujii S, Numata D, Nagai H, et al. Development of ultrafast-response anodized-aluminum pressure-sensitive paints[R]. AIAA-2013-0485, 2013. http://www.researchgate.net/publication/268468032_Development_of_Ultrafast-Response_Anodized-Aluminum_Pressure-Sensitive_Paints
    [41]
    Winslow N A, Carroll B F, Kurdila A J. Model development and analysis of the dynamics of pressure sensitive paints[J]. AIAA Journal, 2001, 39(4):660-666. doi: 10.2514/2.1359
    [42]
    Merienne M C, Coponet D, Luyssen J M. Transient pressure-sensitive paint investigation in a nozzle[J]. AIAA Journal, 2012, 50(50):1453-1461. doi: 10.2514/13050926
    [43]
    Merienne M C, Le Sant Y, Ancelle J, et al. Unsteady pressure measurement instrumentation using anodized-aluminum PSP applied in a transonic wind tunnel[J]. Meas Sci Technol, 2004, 15(15):2349-2360. http://adsabs.harvard.edu/abs/2004MeScT..15.2349M
    [44]
    McGraw C M, Shroff H, Khalil G, et al. The phosphorescence microphone:a device for testing oxygen sensors and films[J]. Rev Sci Instrum, 2003, 74(12):5260-5266. doi: 10.1063/1.1626009
    [45]
    Virgin C A, Carroll B F, Cattafesta L N, et al. Pressure sensitive paint for acoustic pressure fluctuations[C]. Proc 2005 ASME Int Mech Eng Congr Expo, New York, 2005.
    [46]
    Peng D, Jensen C D, Juliano T J, et al. Temperature-compensated fast pressure sensitive paint[J]. AIAA Journal, 2013, 51(10):2420-2431. doi: 10.2514/1.J052318
    [47]
    Klein C, Sachs W E, Henne U, et al. Determination of transfer function of pressure-sensitive paint[R]. AIAA-2010-0309, 2010. doi: 10.2514/6.2010-309
    [48]
    Klein C, Sachs W E, Henne U. et al. Application of pressure-sensitive paint for determination of dynamic surface pressures on a 30 Hz oscillating 2D profile in transonic flow[M]. New York:Springer, 2010.
    [49]
    Gregory J W, Sakaue H, Sullivan J P. Fluidic oscillator as a dynamic calibration tool[R]. AIAA-2002-2701, 2002. doi: 10.2514/6.2002-2701
    [50]
    Sakamura Y, Suzuki T, Matsumoto M. Optical measurements of high-frequency pressure fluctuations using a pressure-sensitive paint and Cassegrain optics[J]. Meas Sci Technol, 2002, 13(10):1591-1598. doi: 10.1088/0957-0233/13/10/312
    [51]
    Jordan J D, Watkins A N, Weaver W L, et al. Sol-gel-based pressure-sensitive paint development[R]. AIAA-99-0566, 1999. doi: 10.2514/6.1999-566
    [52]
    Nakakita K. Scanning unsteady PSP technique for high-frequency and small-pressure fluctuation in low-speed[R]. AIAA-2010-4920, 2010.
    [53]
    Nakakita K. Unsteady pressure measurement on NACA0012 model using global low-speed unsteady PSP technique[R]. AIAA-2011-3901, 2011. doi: 10.2514/6.2011-3901
    [54]
    Yorita D, Nagai H, Asai K, et al. Unsteady PSP technique for measuring naturally-disturbed periodic phenomena[R]. AIAA-2010-0307, 2010. doi: 10.2514/6.2010-307
    [55]
    Asai K, Yorita D. Unsteady PSP measurement in low-speed flow: overview of recent advancement at Tohoku University[R]. AIAA-2011-0847, 2011.
    [56]
    Disotell K J, Gregory J W. Unsteady surface signature of a pulsed vortex generator jet[J]. Vis Journal, 2011, 14(2):121-127. doi: 10.1007/s12650-011-0080-3
    [57]
    Fang S, Disotell K J, Long S R, et al. Application of fast responding pressure-sensitive paint to a hemispherical dome in unsteady transonic flow[J]. Exp Fluids, 2011, 50(6):1495-1505. doi: 10.1007/s00348-010-1010-1
    [58]
    Pastuhoff M, Tillmark N, Alfredsson P H. Wall pressure measurements in a Y-junction at pulsating flow using polymer/ceramic pressure sensitive paint[C]. Proc 10th Int Symp Exp Comput Aerothermodyn Internal Flows, Brussels, 2011.
    [59]
    Singh M, Naughton J W, Yamashita T, et al. Surface pressure and flow field behind an oscillating fence submerged in turbulent boundary layer[J]. Exp Fluids, 2011, 50(3):701-714. doi: 10.1007/s00348-010-0977-y
    [60]
    Kameda M, Seki H, Makoshi T, et al. Unsteady measurement of a transonic delta wing flow by a novel PSP[R]. AIAA-2008-6418, 2008. doi: 10.2514/6.2008-6418
    [61]
    Nakakita K, Osawa J, Hori N, et al. Unsteady pressure-sensitive paint measurement for oscillating shock wave in supersonic nozzle[R]. AIAA-2008-6580, 2008.
    [62]
    Nakakita K, Arizono H. Visualization of unsteady pressure behavior of transonic flutter using pressure-sensitive paint measurement[R]. AIAA-2009-3847, 2009.
    [63]
    Nakakita K, Takama Y, Imagawa K, et al. Unsteady PSP measurement of transonic unsteady flow field around a rocket fairing model[R]. AIAA-2012-2758, 2012. http://www.researchgate.net/publication/268563427_Unsteady_PSP_Measurement_of_Transonic_Unsteady_Flow_Field_around_a_Rocket_Fairing_Model
    [64]
    Crafton J, Forlines A, Palluconi S, et al. Investigation of transverse jet injections in a supersonic crossflow using fast responding pressure-sensitive paint[R]. AIAA-2011-3522, 2011.
    [65]
    Bitter M, Hara T, Hain R, et al. Characterization of pressure dynamics in an axisymmetric separating/reattaching flow using fast-responding pressure-sensitive paint[J]. Exp Fluids, 2012, 53(6):1737-1749. doi: 10.1007/s00348-012-1380-7
    [66]
    Hayashi T, Ishikawa H, Sakaue H. Development of polymer-ceramic pressure-sensitive paint and its application to supersonic flow field[C]. 28th Int Symp ShockWaves, Berlin: Springer, 2012.
    [67]
    Flaherty W, Reedy T M, Elliott G S, et al. Investigation of cavity flow using fast-response pressure sensitive paint[R]. AIAA-2013-0678, 2013. doi: 10.2514/1.J052864
    [68]
    Merienne M C, Le Sant Y, Lebrun F, et al. Transonic buffeting investigation using unsteady pressure-sensitive-paint in a large wind tunnel[R]. AIAA-2013-1136, 2013.
    [69]
    Hird K, Juliano T J, Gregory J W, et al. Study of unsteady surface pressure on a turret via pressure-sensitive paint[C]. AIAA Fluid Dyn Conf, San Diego, CA, 2013. doi: 10.2514/6.2013-3135
    [70]
    Nakakita K. Unsteady pressure distribution measurement around 2D-cylinders using pressure-sensitive paint[R]. AIAA-2007-3819, 2007. http://www.researchgate.net/publication/268561760_Unsteady_Pressure_Distribution_Measurement_around_2D-Cylinders_Using_Pressure-Sensitive_Paint
    [71]
    Sakaue H, Miyamoto K, Miyazaki T. A motion-capturing pressure-sensitive paint method[J]. Appl Phys, 2013, 113(8):084901. doi: 10.1063/1.4792761
    [72]
    Stich M I J, Fischer L H, Wolfbeis O S. Multiple fluorescent chemical sensing and imaging[J]. Chem Soc Rev, 2010, 39(8):3102-3114. doi: 10.1039/b909635n
    [73]
    Gregory J W, Kumar P, Peng D, et al. Integrated optical measurement techniques for investigations of fluid-structure interactions[R]. AIAA-2009-4044, 2009. doi: 10.2514/6.2009-4044
    [74]
    Juliano T J, Kumar P, Peng D, et al. Single-shot, lifetime-based pressure sensitive paint for rotating blades[J]. Meas Sci Technol, 2011, 22(8):085403. doi: 10.1088/0957-0233/22/8/085403
    [75]
    Disotell K J, Juliano T J, Peng D, et al. Unsteady pressure-sensitive paint measurements on an articulated model helicopter in forward flight[R]. AIAA-2012-2757, 2012.
    [76]
    Disotell K J, Juliano T J, Peng D, et al. Single-shot temperature-and pressure-sensitive paint measurements on an unsteady helicopter blade[J]. Exp Fluids, 2014, 55(2):1671. doi: 10.1007/s00348-014-1671-2
    [77]
    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. doi: 10.2514/1.J051167
    [78]
    Watkins A N, Leighty B D, Lipford W E, et al. Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight[R]. AIAA-2012-2756, 2012.
    [79]
    Wong O D, Watkins A N, Goodman K Z, et al. Blade tip pressure measurements using pressure sensitive paint[C]. Proc 68th Am Helicopter Soc Annu Forum Technol Disp, Alexandria, 2012.
    [80]
    Gregory J W, Juliano T J, Disotell K J, et al. Deconvolution-based algorithms for deblurring PSP images of rotating surfaces[R]. AIAA-2013-0484, 2013. http://www.researchgate.net/publication/289183356_Deconvolution-based_algorithms_for_deblurring_PSP_images_of_rotating_surfaces?ev=auth_pub
    [81]
    Goss L, Jones G, Crafton J, et al. Temperature compensation for temporal (lifetime) pressure sensitive paint measurements[R]. AIAA-2005-1027, 2005.
    [82]
    Kimura F, Rodriguez M, McCann J, et al. Development and characterization of fast responding pressure sensitive microspheres[J]. Rev Sci Instrum, 2008, 79(7):074102. doi: 10.1063/1.2952502
    [83]
    Sullivan J P. Temperature and pressure sensitive paint[C]. Lecture Series 2000-2001, Advanced Measurement Techniques, The von Karman Institute for Fluid Mechanics, Belgium, 2001.
    [84]
    Tomac M N, Gregory J W. Jet interactions in a feedback-free fluidic oscillator at low flow rate[C]. AIAA Fluid Dyn Conf, San Diego, CA, 2013. http://www.researchgate.net/publication/269049643_Jet_Interactions_in_a_Feedback-Free_Fluidic_Oscillator_at_Low_Flow_Rate
    [85]
    Crafton J, Forlines A, Palluconi S, et al. Investigation of transverse jet injections in a supersonic crossflow using fast responding pressure-sensitive paint[J]. Exp Fluids, 2015, 56(2):27. doi: 10.1007/s00348-014-1877-3
    [86]
    Xingju X, Minglei Y, Jingbo Y, et al. Fast Response PSP Measurement In a Hypersonic Wind Tunnel[R]. AIAA-2014-2943, 2014. http://www.researchgate.net/publication/281700229_Fast_response_PSP_measurement_in_a_hypersonic_wind_tunnel
    [87]
    Burns S, Sullivan J P. The use of pressure sensitive paints on rotating machinery[C]. Proc 16th Int Cong Instrumentation in Aerospace Simulation Facilities (ICIASF), 1995. http://www.researchgate.net/publication/3655474_The_use_of_pressure_sensitive_paints_on_rotating_machinery
    [88]
    Mosharov V E, Radchenko V N, Fonov S D. Luminescent pressure sensors in aerodynamic experiments[R]. TsAGI 8805, 1997.
    [89]
    Hubner J P, Abbitt J D, Carroll B F. Pressure measurements on rotating machinery using lifetime imaging of pressure sensitive paint[R]. AIAA-96-2934, 1996. http://www.researchgate.net/publication/268457406_Pressure_measurements_on_rotating_machinery_using_lifetime_imaging_of_pressure_sensitive_paint
    [90]
    Disotell K J, Peng D, Juliano T J, et al. Single-shot temperature-and pressure-sensitive paint measurements on an unsteady helicopter blade[J]. Exp Fluids, 2014, 55(2):1671. doi: 10.1007/s00348-014-1671-2
    [91]
    Peng D, Lingrui J, Yuelong Y, et al. Single-shot lifetime-based PSP and TSP measurements on turbocharger compressor blades[J]. Exp Fluids, 2017, 58(9):127. doi: 10.1007/s00348-017-2416-9
    [92]
    Ishii M, Yamada M, Miyazaki T, et al. Pressure/temperature measurement of a free-flight object by PSP/TSP[R]. AIAA-2014-2542, 2014. doi: 10.2514/6.2014-2542
    [93]
    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]. Exp Fluids, 2016, 57(4):45. doi: 10.1007/s00348-016-2130-z
    [94]
    Nakakita K, Yamazaki T, Asai K, et al. Pressure sensitive paint measurement in a hypersonic shock tunnel[R]. AIAA-2000-2523, 2000. doi: 10.2514/6.2000-2523
    [95]
    Gardner A D, Klein C, Sachs W E, et al. Investigation of three-dimensional dynamic stall on an airfoil using fast-response pressure-sensitive paint[J]. Exp Fluids, 2014, 55(9):1807. doi: 10.1007/s00348-014-1807-4
    [96]
    Neal Watkins A, Bradley D Leighty, William E Lipford, et al. Applying pressure sensitive paint technology to rotor blades[R]. NASA/TM-2014-218259, 2014. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20140006409.pdf
    [97]
    Jingbo Y, Zhan H, Yipeng R, et al. Investigation of unsteady pressure measurement and visualization using fast response PSP[C]. The 14th Asian Symposium on Visualization, Beijing, 2017.
  • 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(24)  / Tables(1)

    Article Metrics

    Article views (299) PDF downloads(19) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return