Temperature- and pressure-sensitive luminescent paints in aerodynamics

Applied Mechanics Reviews

Volumn 50, Issue 4, 1997, Pages 227-246

  Liu, Tianshu ^a   Campbell, B T ^a   Burns, S P ^a   Sullivan, J P ^a  

^a PURDUE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; LUMINESCENCE; PRESSURE EFFECTS; THERMAL EFFECTS;

PRESSURE SENSITIVE PAINT (PSP); TEMPERATURE SENSITIVE PAINT (TSP);

LUMINOUS PAINT;

EID: 0031120380     PISSN: 00036900     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.3101703     Document Type: Article

References (112)

1. Alaruri S, McFarland D, Brewington A, Thomas M, and Sallee N (1995), Development of a fiber-optic probe for thermographic phosphor measurements in turbine engines, Optics and Lasers in Eng 22, 17-31.
2. Ardasheva MM, Nevskii LB, and Pervushin GE (1985), Measurement of pressure distribution by means of indicator coatings, J Appl Mech Tech Phys, n 4, 24-33.
3. Asai K, Kanda H, Kunimasu T, Liu T, and Sullivan J (1996), Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint, AIAA Paper 96-2185.
4. Babinsky H and Edwards JA (1993), Application and analysis of liquid crystal thermographs in short duration hypersonic flow, AIAA Paper 93-0182.
5. Baron AE, Danielson JD, Gouterman M, Wan J, Callis JB, and McLachlan B (1993), Submillisecond response times of oxygen-quenching luminescent coatings, Rev Sci Instrum 64(12), 3394-3402.
6. Becker RS (1969), Theory and Interaction of Fluorescence and Phosphorescence, Wiley Interscience, New York.
7. Bell JH and McLachlan BG (1993), Image registration for luminescent paint sensors, AIAA Paper 93-0178.
8. Bennett RG (1960), Instrument to measure fluorescence lifetimes in the millimicrosecond region. Rev Sci Instrum 31(12), 1275-1279.
9. Bennett RG and McCartin PJ (1966), Radiationless deactivation of the fluorescent state of substituted anthracences, J Chem Phys, 44 (5) 1969-1973.
10. Birch DJS and Imhof RE (1991), Time-domain fluorescence spectroscopy using time-correlated single-photon counting, topics in Fluorescence Spectroscopy, Volume I: Techniques, edited by JR Lakowicz, Plenum Press, New York, Ch 1.
11. Borovoy V, Bykov A, Mosharov V, Orlov A, Radchenko V, and Phonov S (1995), Pressure sensitive paint application in shock wind tunnel, Proc 16th Int Congress Instrumentation in Aerospace Simulation Facilities (.ICIASF), IEEE, Wright-Patterson AFB, Dayton OH, 34.1-34.4.
12. Bradley LC (1953), Temperature-sensitive phosphor used to measure surface temperature in aerodynamics, Rev Sci Instrum 24(3), 219-220.
13. Brody SS (1957), Instrument to measure fluorescence lifetimes in the millimicrosecond region, Rev Sci Instrum 28(12), 1021-1026.
14. Buck GM (1988), Imaging system for quantitative surface temperature mapping using two-color thermographic phosphors, presented at 34th Int Instrumentation Symp, Albuquerque NM.
15. Buck GM (1989), Automated thermal mapping techniques using chromatic image analysis, NASA TM 101554.
16. Buck GM (1991), Surface temperature/heat transfer measurement using a quantitative phosphor thermography system, AIAA Paper 91-0064.
17. Buck GM (1994), Simultaneous luminescence pressure and temperature measurements on dyed ceramic models for hypersonic wind tunnels, AIAA Paper 94-2482.
18. Bugos AR (1989), Characterization of the emission properties of thermographic phosphors for use in high temperature sensing applications, MS Thesis, Univ of Tennessee, Knoxville TN.
19. Bukov AP, Orlov AA, Mosharov VE, Radchenko VN, and Pesetsky VA (1992), Application of luminescence quenching for pressure field measurements on the model surface in wind tunnel, Proc Wind Tunnels and Wind Tunnel Test Techniques Conf Royal Aeronaut Soc, London, UK, 8.1-8.11.
20. Bukov A, Mosharov V, Orlov A, Pesetsky V, Radchenko V, Phonov S, Matyash S, Kuzmin M, and Sadovsky N (1993), Optical surface pressure measurements: accuracy and application field evaluation, 73th AGARD Fluid Dynamics Panel Meeting and Symp on Wall Interference, Support Interference, and Flow Field Measurements, Brussels, Belgium.
21. Burns S (1995), Fluorescent pressure sensitive paints for aerodynamic rotating machinery, MS Thesis, Sch of Aeronaut and Astronaut, Purdue Univ, W Lafayette IN.
22. Burns S and Sullivan J (1995), Use of pressure sensitive paints on rotating machinery, Proc 16th Int Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, Wright-Patterson AFB, Dayton OH, 32.1-32.14.
23. Campbell B, Liu T, and Sullivan J (1992), Temperature measurement using fluorescent molecules, 6th Int Symp Appl Laser Tech Fluid Mech, Lisbon, Portugal.
24. Campbell B (1993), Temperature sensitive fluorescent paints for aerodynamics applications, MS Thesis, Sch of Aeronaut and Astronaut, Purdue Univ, W Lafayette IN.
25. Campbell B, Liu T, and Sullivan J (1994), Temperature sensitive fluorescent paint systems, AIAA Paper 94-2483.
26. Carroll BF, Winslow A, Abbitt J, Schanze K, and Morris M (1995), Pressure sensitive paint: application to a sinusoidal pressure fluctuation, 16th Int Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, Wright-Patterson AFB, Dayton OH, 35.1-35.6.
27. Carroll BF, Abbitt JD, Lukas EW, and Morris MJ (1996), Step response of pressure sensitive paints, AIAA J, 34(3) 521-526.
28. Cattafesta III LN and Moore JG (1995), Uncertainty estimates for luminescent temperature-sensitive paint intensity measurements, AIAA Paper 95-2193.
29. Coyle LM, Bullock JP, and Gouterman M (1995), Interfacial effects at the basecoat-psp boundary, abstract of workshop on pressure, temperature and shear sensitive coatings, Univ of Florida, Gainesville FL.
30. Crites BC (1993), Measurement techniques: Pressure sensitive paint technique, Lecture Series 1993-05, von Karman Inst for Fluid Dynamics.
31. Crovini L and Fernicola V (1992), Oven to test fluorescent-decay temperature sensor, Sensors and Actuators B 7 529-532.
32. Czysz P and Dixon WP (1969), Quantitative heat transfer measurement using thermographic phosphors, SPIE J 7(3) 77-79.
33. Davies AG, Bedwell D, Dunleavy M, and Brownjohn N (1995), Pressure sensitive paint measurements using a phosphorescence lifetime method, presented at 7th Int Symp on Flow Visualization, Sept 11-14, Seattle WA.
34. Dolling DS and Bogdonoff SM (1981), Scaling of interactions of cylinders with supersonic turbulent boundary layers, AIAA J 19(5), 655-657.
35. Donovan JF (1992), Preliminary results from a trangentially injected shock wave/turbulent boundary layer interaction, presented at 13th Symp on Turbulence, Rolla MO.
36. Donovan JF, Morris MJ, Pal A, Benne ME, and Crites RC (1993), Data analysis techniques for pressure- and temperature-sensitive paint, AIAA Paper 93-0176.
37. Dowgwillo RM, Morris MJ, Donovan JF, and Benne ME (1994), Application of the pressure sensitive paint technique to high speed wind tunnel testing of a fighter aircraft configuration with complex store loadings, AIAA Paper 94-1932.
38. Engler RH, Hartmann K, and Schultze B (1991a), Aerodynamic assessment of an optical pressure measurement system (OPMS) by comparison with conventional pressure measurements in a high speed wind tunnel, Proc 14th Int Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, Rockville MD, 17-24.
39. Engler RH, Hartmann K, Troyanovski I, and Vollan A (1991b), Description and assessment of a new optical pressure measurement system (OPMS) demonstrated in the high speed wind tunnel of dir in Gottingen, DLR Report DLR-FB 92-124.
40. Engler RH (1995), Further developments of pressure sensitive paint (OPMS) for non flat models in steady transonic flow and unsteady conditions, Proc 16th Int Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, Wright-Patterson AFB, Dayton OH, 33.1-33.8.
41. Everett DE, Dutton JC, and Morris MJ (1995), Pressure sensitive paint measurements of the pressure field about a sonic jet injected transversely into a Mach 1.6 free stream, AIAA Paper 95-0524.
42. Fried JR (1995), Polymer Science and Technology, Prentice Hall, New York.
43. Gallery JM (1993), Luminescence imaging for aerodynamic temperature and pressure measurements, PhD Thesis, Dept of Chem, Univ of Washington, Seattle WA.
44. Gartenburg E and Robert AS (1991), Twenty-five years of aerodynamic research with infrared imaging, a survey, presented at Thermosense XIII, Int Conf Thermal Applications and Image Diagnostic, Orlando FL.
45. Gewehr PM and Delpy DT (1993), Optical oxygen sensor based on phosphorescence lifetime quenching and employing a polymer immobilised metalloporphyrin probe, Medical and Biological Engg and Computing, January, 2-21.
46. Gord JR, Buckner SW, and Weaver WL (1995), Dissolved oxygen quantitation in fuel through measurements of dynamically quenched fluorescence lifetime, Proc 16th Int Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, Wright-Patterson AFB, Dayton OH, 39.1-39.6.
47. Gouterman M, Callis J, Burns D, Kavandi J, Gallery J, Khalil G, Green E, McLachlan B, and Crowder J (1990), Luminescence imaging for aerodynamic testing, Proc of ONR/NASA Workshop on Quantitative Flow Visualization, J Sullivan and B Holmes (eds), Purdue Univ, W Lafayette IN.
48. Grattan KTV, Palmer AW, and Willson CA (1987), Miniaturised microcomputer-based neodymium’decay-time’ temperature sensor, J Phys E: SciInstrum 20, 1201-1205.
49. Hamner M, Campbell B, Liu T, and Sullivan J (1994), Scanning laser system for temperature and pressure sensitive paint, AIAA Paper 94-0728.
50. Harris J and Gouterman M. (1995), Referenced pressure sensitive paint, flow visualization VII, Proc of 7th Int Symp on Flow Visualization, J Crowder (ed), Seattle WA, p.802.
51. Hartmann P, Leiner MJP, and Lippitsch ME (1995), Response characteristics of luminescent oxygen sensors, Sensors and Actuators B 29 251 -257.
52. Hippensteele SA, Russel LM, and Stepka FS (1983), Evaluation of a method for heat transfer measurements and thermal visualization using a composite of a heater element and liquid crystals, ASME J Heat Transfer 105 184-189.
53. Hippensteele SA, Russel LM, and Torres FJ (1985), Local heat-transfer measurements on a large scale-model turbine blade airfoil using a composite of a heater element and liquid crystals, J Eng Gas Turbines Power 107 953-960.
54. Hubner JP, Abbitt JD, and Carroll BF (1996), Pressure measurements on rotating machinery using lifetime imaging of pressure sensitive paint, AIAA Paper 96-2934.
55. Kavandi J, Callis JB, Gouterman MP, Khalil G, WrightD, Green E, Burns D, and McLachlan B (1990), Luminescent barometry in wind tunnels, Rev Sci Instrum 61(11) 3340-3347.
56. Kolodner P and Tyson A (1982), Microscope fluorescent imaging of surface temperature profiles with 0.01 C resolution, Appl Phys Lett 40(9) 782-784.
57. Kolodner P and Tyson A (1983a), Remote thermal imaging with 0.7 micron spatial resolution using temperature dependent fluorescent thin films, Appl Phys Lett 42(1) 117-119
58. Kolodner P and Tyson A (1983b), Non-contact surface temperature measurement during reactive-ion etching using fluorescent polymer films, Appl Phys Lett 42(8) 749-751.
59. Krevelen DWV (1976), Properties of Polymers, Elsevier, New York.
60. Lee Y and Settles GS (1992), Heat transfer measurements and CFD comparison of swept shock/boundary-layer interactions, AIAA Paper 923665.
61. Liu T, Campbell T, and Sullivan J (1992), Thermal paints for shock/boundary layer interaction in inlet flows, AIAA Paper 92-3626.
62. Liu T, Campbell B, and Sullivan J (1994a), Surface temperature of a hot film on a wall in shear flow, Int J Heat Mass Transfer, 37 (17) 2809-2814.
63. Liu T, Campbell B, and Sullivan J (1994b), Remote surface temperature and heat transfer mapping for a waverider model at Mach 10 using fluorescent paint, AIAA Paper 94-2484.
64. Liu T, Campbell B, and Sullivan J (1995a), Fluorescent paint for measurement of heat transfer in shock-turbulent boundary layer interaction, Exp Thermal Fluid Sci 10 101-112.
65. Liu T, Campbell T, Sullivan J, Lafferty J, and Yanta W (1995b), Heat transfer measurement on a waverider at Mach 10 using fluorescent paint, J Thermophys Heat Transfer 9(4) 605-611.
66. Liu T, Campbell B, and Sullivan J (1995c), Accuracy of temperaturesensitive fluorescent paint for heat transfer measurements, AIAA Paper 95-2042.
67. Liu T and Sullivan J. (1996a), Heat transfer and flow structures in an excited circular impinging jet, Int J Heat Mass Transfer, 39(17) 3695-3706.
68. Liu T (1996b), Applications of temperature-sensitive luminescent paints in aerodynamics, PhD Thesis, Sch of Aeronaut and Astronaut, Purdue Univ, W Lafayette IN.
69. Liu T, Johnston R, Torgerson S, Fleeter S, and Sullivan J (1997), Rotor blade pressure measurement in a high speed axial compressor using pressure and temperature sensitive paints, AIAA Paper 97-0162
70. MacCraith BD, McDonagh CM, Keeffe GO, McEvoy AK, Butler T, and Sheridan FR (1995), Sol-Gel coatings for optical chemical sensors and biosensors, Sensors and Actuators B 29 51 -57.
71. McLachlan BG, Kavandi JL, Callis JB, Gouterman M, Green E, and Khalil G (1993a), Surface pressure field mapping using luminescent coatings, Exp Fluids 14 33-41.
72. McLachlan BG, Bell JH, Gallery J, Gouterman M, and Callis J (1993b), Boundary layer transition detection by luminescence imaging, AIAA Paper 93-0177.
73. McLachlan BG and Bell JH (1995a), Pressure-sensitive paint in aerodynamic testing, Exp Thermal Fluid Sci 10 470-485.
74. McLachlan BG, Bell JH, Park H, Kennelly RA, Schreiner JA, Smith SC, Strong JM, Gallery J, and Gouterman M (1995b), Pressure-sensitive paint measurements on supersonic high-sweep oblique wing model, J Aircraft 32(2) Mar-Apr, 217-227.
75. Meier B, Werner T, Klimant I, and Wolfbeis OS (1995), Novel oxygen sensor material based on a ruthenium bipyridyl complex encapsulated in zeolite Y: Dramatic differences in the efficiency of luminescence quenching by oxygen on going from surface-adsorbed to zeolite-encapsulated fluorophores, Sensors and Actuators B 29 240-245.
76. Morris MJ, Benne ME, Crites RC, and Donovan JF (1993a), Aerodynamics measurements based on photoluminescence, AIAA Paper 93-0175.
77. Morris MJ, Donovan JF, Kegelman JT, Schwab SD, Levy RL, and Crites RC (1993b), Aerodynamic applications of pressure sensitive paint, AIAA J Vol. 31(3) March, 419-425.
78. Morris MJ (1995), Use of pressure-sensitive paints in low-speed flows, Proc 16th Int Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, Wright-Patterson AFB, Dayton OH, 31.131.10.
79. Mulder M (1991), Basic Principles of Membrane Technology, Kluwer Academic Publ, Boston.
80. Noel BW et al (1985), Proposed method for remote thermometry in turbine engines, AIAA Paper 85-1468.
81. Noel BW et al (1986), Proposed laser-induced fluorescence method for remote thermometry in tuibine engines, J Propulsion Power 2(6) 565
82. Noel BW et al (1987), Evaluation and testing thermographic phosphors for turbine-engine temperature measurements, AIAA Paper 87-1761.
83. Oglesby DM, Puram CK, and Upchurch BT (1995a), Optimization of measurements with pressure sensitive paints, NASA TM 4695.
84. Oglesby DM, Leighty BD, and Upchurch BT (1995b), Pressure sensitive paint with an internal reference luminiphore, Proc of 41st Int Instrumentation Symp, Instrument Soc of Am, Denver CO, 381-395.
85. Oglesby DM, Upchurch BT, Leighty BD, and Simmons KA (1996), Pressure sensitive paint with internal temperature sensing luminiphore, Proc of 42nd Int Instrumentation Symp, Instrument Soc of Am, San Diego CA.
86. Papkovsky DB (1995), New oxygen sensors and their application to biosensing, Sensors and Actuators B 29, 213-218.
87. Parker CA (1968), Photoluminescence of Solutions, Elsevier Publ, New York.
88. Peterson JI and Fitzgerald RV (1980), New technique of surface flow visualization based on oxygen quenching of fluorescence, Rev Sci Instrum 51(5), 670-671.
89. Rabek JF (1987), Mechanisms of Photophysical Processes And Photochemical Reactions In Polymer: Theory and Applications, John Wiley and Sons, New York.
90. Robinson PA and Perlmutter DD (1994), Oxygen diffusion and reaction of residual carbon in sol-gel-derived silica xerogel, J Non-Crystalline Solids 169 183-199.
91. Rodi PE and Dolling DS (1992), Experimental/computational studies of sharp fin induced shock/turbulent boundary layer interactions at Mach 5: Experimental results, AIAA Paper 92-0749.
92. Romano V, Zweig AD, Frenz M, and Weber HP (1989), Time-resolved thermal microscopy with fluorescent films, Appl Phys B49 527-533.
93. Sacksteder L, Demas JN, and DeGraff BA (1993), Design of oxygen sensors based on quenching of luminescent metal complexes: Effect of ligand size on heterogeneity, Anal Chem 65(23) Dec, 3480-3483.
94. Sajben M (1993), Uncertainty estimates for pressure sensitive paint measurements, J, Vol. 31(11) 2105-2110.
95. Schultz DL and Jones TV (1973), Heat transfer measurements in short-duration hypersonic facilities, AGARDograph No 165.
96. Sellers ME and Brill JA (1994), Demonstration test of pressure sensitive paint in the aedc 16-ft transonic wind tunnel using the TST model, AIAA Paper 94-2481.
97. Settles GS and Lu FK (1985), Conical similarity of shock/boundary-layer interactions generated by swept and unswept fins, AIAA J, Vol. 23(7) 1021-1027.
98. Sholes RR and Small JG (1980), Fluorescent decay thermometer with biological applications, Rev Sci Instrum 51(7), 882-884.
99. Song L and Fayer MD (1991), Temperature dependent intersystem crossing and triplet-triplet absorption of rubrene in solid solution, J Luminescence 50 75-81
100. Sullivan JP (1991), Surface temperature measurement using fluorescent molecules, Lecture Notes, Purdue Univ.
101. Szmacinski H and Lakowicz JR (1995), Fluorescence lifetime-based sensing and imaging, Sensors and Actuators B 29, 16-24.
102. Tobin KW, Allison SW, Cates MR, Capps GJ, Beshears DL, Cyr M, and Noel BW (1990), High-temperature phosphor thermometry of rotating turbine blades, AIAA J Vol. 28(8) 1485-1490.
103. Torgerson SD, Liu T, and Sullivan JP (1996), Use of pressure sensitive paints in low speed flows, AIAA Paper 96-2184.
104. Torgerson SD (1996), Laser scanning system for use with pressure and temperature sensitive paints, MS Thesis, Sch of Aeronaut and Astronaut, Purdue Univ, W Lafayette IN (to appear).
105. Troyanovsky I, Sadovskii N, Kuzmin M, Mosharov V, Orlov A, Radchenko V, and Phonov S (1993), Set of luminescence pressure sensors for aerospace research. Sensors and Actuators B11 201-206.
106. Uibel R, Khalil G, Gouterman M, Gallery J, and Callis J (1993), Video luminescent barometry: The induction period, AIAA Paper 93-0179.
107. 2-pulsed laser, Indian J Pure and Appi Phys 25 Feb, 72-76.
108. Volan A and Alati L (1991), New optical pressure measurement system, Proc I4lh Ini Congress Instrumentation in Aerospace Simulation Facilities (ICIASF), IEEE, New York, 10-16.
109. Wan J (1993), Fast response luminescent pressure sensitive coating and derivatives of tetra (pentafluorophenyl) porpholactone, PhD Thesis, Dept of Chem, Univ of Washington, Seattle WA.
110. Wickersheim K and Sun M (1985), Phosphors and fiber optics remove doubt from difficult temperature measurements, Research and Development Nov, 114-119.
111. Winslow NA, Carroll BF, and Setzer FM (1996), Frequency response of pressure sensitive paints, AIAA Paper 96-1967.
112. Xu W, McDonough RC, Langsdorf B, Demas JN, and DeGraff BA (1994), Oxygen sensors based on luminescence quenching: Interactions of metal complexes with the polymer supports, Anal Chem 66(23) Dec 4133-4141.