Volume 21 Issue 2
Apr.  2006
Turn off MathJax
Article Contents
LIU Bo, ZHOU Qiang, JIN Jun, MA Chang-you. Applications of Pressure-Sensitive Paint Technique[J]. Journal of Aerospace Power, 2006, 21(2): 225-233.
Citation: LIU Bo, ZHOU Qiang, JIN Jun, MA Chang-you. Applications of Pressure-Sensitive Paint Technique[J]. Journal of Aerospace Power, 2006, 21(2): 225-233.

Applications of Pressure-Sensitive Paint Technique

  • Received Date: 2005-06-26
  • Rev Recd Date: 2005-12-20
  • Publish Date: 2006-04-28
  • Since 1980’s,with the development of Biochemistry,Photophysics,Computer & Information Technology and Image-processing technology,Pressure-Sensitive Paint(PSP) technique has been widely employed in many engineering fields because of its evident advantages,such as easy to operate,lower cost,noninterference in flow field and wide range of pressure measurement.The contents of this paper including basic theory of luminescence molecules and its application to optical measurement,development of PSP technique,applications of PSP technique both to internal and external flow fields were depicted to exhibit the perspectives of PSP technique.The details of the differences of PSP technique applied to internal and external flow fields,the role of Temperature-Sensitive Paint in PSP measurement,the methods and procedures of PSP technique application were introduced as many as possible.

     

  • loading
  • [1]
    Sexton M R,O'Brien W F,Moses H L.An on Rotor Investigation of Rotating Stall in an Axial Compressor[R].Defense Technical Information Center (DTIC) Technical Report,Cameron Station,Alexandria,VA,1973:33.1 ~ 10.
    [2]
    Peterson J I,Fitzgerald V F.New Technique of Surface Flow Visualization Based on Oxygen Quenching of Fluorescence[J].Rev.Sci.Instrum.,1980,51 (5):670~671.
    [3]
    Morris M J.Use of Pressure-Sensitive Paints in Low Speed Flows[A].CH34827-95,IEEE 16th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF)[C].Wright-Patterson AFB,OH,1995:31.1~10.
    [4]
    Bukov A P,Orlov A A,Mosharov V E,Radchenko V N,Pesetsky V A,Sorokin A V,Phonov S D,Alaty L,Colucci V.Application of Luminescent Quenching for Pressure Field Measurements on the Model Surface in a Wind Tunnel[R].Wind Tunnels and Wind Tunnel Test Techniques,The Royal Aeronautical Society,Southhampton University,United Kingdom,September,1992.
    [5]
    Bukov A,Mosharov V,Orlov A,Pesetsky V,Radchenko V,Phonov S,Matyash S,Kuzmin M,Sadozsky N.Optical Surface Pressure Measurements:Accuracy and Application Field Evaluation[A].73rd AGARD Fluid Dynamics Panel Meeting and Symposium on Wall Interference,Support Interference,and Flow Field Measurements[C].Brussels,Belgium,1993.
    [6]
    Kelly R Navarra.Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications[R].Thesis for Master Degree of Virginia Polytechnic Institute and State University,Blacksbur g,Virginia,1997.
    [7]
    Troyanovsky I,Sadocskii N,Kuzmin M,Mosharov V,Orlov A,Radchenko V,Phonov S.Set of Luminescence PressureSensors for Aerospace Research[J].Sens.And Act.,1993,11:201~206.
    [8]
    Volan A,Alafi L.New Optical Pressure Measurement System[A].IEEE 14th International Congress of Instrumentation in Aerodynamic Simulation Facilities (ICIASF)[C].New York:1991:10~16.
    [9]
    Engler R H.Further Developments of Pressure Sensitive Paint (OPMS) for Non-Flat Models in Steady Transonic Flow and Unsteady Conditions[A].CH34827-95,IEEE 16th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF)[C].Wright-Patterson AFB,OH,1995:33.1~8.
    [10]
    Luminescent Pressure Sensors (LPS) and Luminescent Pressure Sensitive Paints (PSP)[R].OPTROD Ltd.,Dugin Str.17~31,Zhukovsky,Moscow reg.,140160 Russia,1995.
    [11]
    Davies A G,Bedwell D,Dunleavy M,Brownjohn N.Pressure Sensitive Paint Measurements Using Phosphorescence Lifetime Method[A].7th International Symposium on Flow Visualization[C].Seattle,WA,1995.
    [12]
    Gouterman M,Callis J,Burns D,Kavandi J,Gallery J,Khalil G,Green E,McLachlan B,Crowder J.Luminescence Imaging for Aerodynamic Testing[A].ONR/NASA Workshop on Quantitative Flow Visualization[C].J.Sullivan and B.Holmes (Eds.),Purdue University,West Lafayette,IN,1990.
    [13]
    Harris J,Gouterman M.Referenced Pressure Sensitive Paint for Flow Visualization Ⅶ[A].7th International Symposium on Flow Visualization[C].Seattle,WA,1995.
    [14]
    McLachlan B G,Bell J H.Pressure-Sensitive Paint in Aerodynamic Testing[J].Exp.Thermal Fluid Sci.,1995,10:470~485.
    [15]
    Pressure-Sensitive Paint:A New Development Tool[J].MCAIR Digest,1992,29(3):.
    [16]
    Burns S,Sullivan J.The Use of Pressure Sensitive Paint on Rotating Machinery[A].CH34827-95,IEEE 16th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF)[C].Wright-Patterson AFB,OH,1995:32.1~14.
    [17]
    Liu T,Johnston R,Torgerson S,Fleeter S,Sullivan J.Rotor Blade Pressure Measurement in a High Speed Axial Compressor using Pressure and Temperature Sensitive Paints[A].AIAA Paper No.97-0162,AIAA 35th Aerospace Sciences Meeting and Exhibit[C].Reno,NV,1997.
    [18]
    Jagharhi A J,Mitchell M,Burkett C,Sealey S.Wind Tunnel Application of Pressure Sensitive Paints at NASA Langley Research Center (8 foot TPT & 7' x10' HST)[R].NASA LaRC IRD ATMB,NASA Langley Research Center,Hampton,VA,1993.
    [19]
    Oglesby D M,Upchurch B T,Leighty B D,Simmons K A.Pressure Sensitive Paint with Internal Temperature Sensing Lumiphore[A].42nd International Instrumentation Symposium,Instrument Society of America[C].San Diego,CA,1996.
    [20]
    Hubner J P,Abbitt J D,Carroll B F.Pressure Measurements on Rotating Machinery using Lifetime Imaging of Pressure Sensitive Paint[A].AIAA Paper No.96-2934,32nd A IAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit[C].Orlando,FL,1996.
    [21]
    Bencic T.Experiences Using Pressure-Sensitive Paint in NASA Lewis Research Center Propulsion Test Facilities[A].AIAA Paper No.95-2831,31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit[C].San Diego,CA,1995.
    [22]
    Torgerson S,Liu T,Sullivan J.Use of Pressure-Sensitive Paints in Low-Speed Flows[A].19th AIAA Advanced Measurement and Ground Testing Technology Conference[C].New Orleans,LA,1995.
    [23]
    Liu Y S,Ware W R.Photophysics of Polycyclic Aromatic Hydrocarbons Absorbed on Silica Gel Surfaces.1.Fluorescence Lifetime Distribution Analysis:An Ⅲ-Conditioned Problem[J].J.Phys.Chem.,1993,97:5980~ 5986.
    [24]
    Popernack T G Jr.,Owens L R,Wahls R A,Hamner M P.Using Temperature Sensitive Paint Technology[A].40th Aerospace Sciences Meeting & Exhibit[C].Nevada,USA,2002.
    [25]
    Donald M Oglesby,Chith K Puram,Billy T Upchurch.Optimization of Measurements with Pressure Sensitive Paints[R].NASA Technical Memorandum 4695,1995.
    [26]
    Tianshu Liu,Norikazu Teduka,Masaharu KamedaKeisuke Asai.Diffusion Time-Scale of Porous Pressure-Sensitive Paint[J].AIAA Journal,2001,39 (12):2400~ 2402.
    [27]
    Danny R Sprinkle,Clifford J Obara,Tahani R Amer,Bradley D Leighty,Michael T Carmine,Cecil G Burkett,Bradley S Sealey.Langley 16-Ft Transonic Tunnel Pressure Sensitive Paint System[R].NASA/TM-2001-211017,NASA,2001.
    [28]
    Amer T R,Liu T,Oglesby D M.Characterization of Pressure Sensitive Paint Intrusiveness Effects on Aerodynamic Data[A].AIAA,2001-0556,39th AIAA Aerospace Sciences Meeting & Exhibit[C].Reno,Nevada,2001.
    [29]
    Martin Gouterman1,James Callis,Larry Dalton,Gamal Khalil,Youssef M'ebarki,Kevin R Cooper,Michel Grenier.Dual Luminophor Pressure-Sensitive Paint:Ⅲ -Application to Automotive Model Testing[J].Measurement and Technology,2004,15:1986 ~ 1994.
    [30]
    Lepicovsky J,Bencic T J.Use of Pressure-Sensitive Paint for Diagnostics in Turbomachinery Flows with Shocks[J].Experiments in Fluids,2002,33:531 ~ 538.
    [31]
    Venkatakrishnan L.Comparative Study of Different Pressure-Sensitive-Paint Image Registration Techniques[J].AIAA Journal,2004,42(11):2311~2319.
    [32]
    Robert M Hall,Shawn H Woodson.Introduction to the Abrupt Wing Stall Program[J].AIAA Journal,2004,41(3):425~435.
    [33]
    David M Schuster,James E Byrd.Transonic Unsteady Aerodynamics of the F/A-18E under Condition Promoting Abrupt Wing Stall[J].AIAA Journal,2004,41 (3):485~491.
    [34]
    Drouillard Ⅱ T F,Linne M A.Luminescence Lifetime Reponse of Pressure-Sensitive Paint to a Pressure Transient[J].AIAA Journal,2005,43(5):1100~1107.
    [35]
    Wim Ruyten.Assimillation of Physical Chemistry Models for Lifetime of Pressure-Sensitive Paint[J].AIAA Journal,2005,43 (3):465 ~ 471.
    [36]
    Channa RAju,Viswanath P R.Pressure-Sensitive Paint in a Blowdown wind Tunnel[J].AIAA Journal,2005,42 (4):908~915.
  • 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

    Article Metrics

    Article views (1834) PDF downloads(550) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return