| [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.
|