Development of Rapid Technology Assessment Tools a New Paradigm in Aerodynamic Design

Proceedings of the International Instrumentation Symposium

Volumn 49, Issue , 2003, Pages 351-380

  Jordan, Jeffrey D ^a   Watkins, A Neal ^a   Fleming, Gary A ^a   South, Bruce W ^a   Leighty, Bradley D ^a   Schwartz, Richard J ^a   Oglesby, Donald M ^a   Ingram, JoAnne L ^a   Tominack, Bonnie J ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Global measurements; Optical diagnostics; Pressure sensitive paint, PSP; Projection moir interferometry, PMI; Unified instrumentation; Virtual diagnostics interface, ViDI; Wind tunnel testing

Indexed keywords

GLOBAL MEASUREMENTS; OPTICAL DIAGNOSTICS; PRESSURE SENSITIVE PAINT (PSP); UNIFIED INSTRUMENTATION; VIDI; VIRTUAL DIAGNOSTICS INTERFACE; WIND TUNNEL TESTING;

AERODYNAMICS; DATA REDUCTION; INTERFACES (COMPUTER); INTERFEROMETRY; PRODUCT DESIGN; VIRTUAL REALITY; WIND TUNNELS;

AEROSPACE VEHICLES;

EID: 1642471227     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (129)

1. R.J. Schwartz, "Virtual Facilities: Imaging the Flow," Aerospace America, July 1995, pages 23 - 26.
2. The National Center for Supercomputing Applications home page for HDF: http://hdf.ncsa.uiuc.edu/.
3. E. Newcomber, Understanding Web Services, XML, WSDL, SOAP and UDDI, Addison-Wesley, 2002. ISBN 0-201-75081-3.
4. D. Dalvi et al., Professional XML for .Net Developers, Wrox Press Ltd., 2001. ISBN 1-861005-31-8.
5. K. Patorski, Handbook of the Moiré Fringe Technique, Elsevier Science Publishers, 1993. pp. vii - xi, pp. 372-373.
6. M.R. Waszak, L.N. Jenkins and P. Ifju, "Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle", AIAA Paper No. AIAA-2001-4005, Presented at the AIAA Atmospheric Flight Mechanics Conference, Montreal, Canada, August 6-9, 2001.
7. G.A. Fleming and S.A. Gorton, "Measurement of Rotorcraft Blade Deformation Using Projection Moiré Interferometry," Journal of Shock and Vibration, Vol. 7, No. 3, 2000.
8. th Annual Forum, Montreal, Canada, June 11-13, 2002.
9. G.A. Fleming, S.M. Bartram, M.R. Waszak and L.N. Jenkins, "Projection Moiré Interferometry Measurements of Micro Air Vehicle Wings," Proceedings of SPIE, Vol. 4448, pp. 90 - 101, 2001.
10. G.A. Fleming and A.W. Burner, "Deformation Measurements of Smart Aerodynamic Surfaces," Proceedings of SPIE, Vol. 3783, pp. 228 - 238, 1999.
11. J.L. Florance, et al., "Contributions of the NASA Langley Research Center to the DARPA/AFRL/NASA/Northrop Grumman Smart Wing Program," AIAA Paper No. AIAA-2003-1961, AIAA Dynamics Specialists Conference, Norfolk, VA, April 7-10, 2003.
12. nd Aerodynamic Measurement Technology and Ground Testing Conference, St. Louis, MO, June 24 - 26, 2002.
13. J.I. Peterson and V.F. Fitzgerald, "New Technique of Surface Flow Visualization Based on Oxygen Quenching of Fluorescence," Review of Scientific Instruments, 51 (5), May 1980, pp. 133-136.
14. B.C. Crites, (1993), "Measurement Techniques- Pressure Sensitive Paint Technique," Lecture Series 1993-05, von Karman Institute for Fluid Dynamics.
15. B.G. McLachlan and J.H. Bell, (1995a), "Pressure-Sensitive Paint in Aerodynamic Testing," Experimental Thermal and Fluid Science, 10, 470-485.
16. B.G. McLachlan, J.L. Kavandi, J.B. Callis, M. Gouterman, E. Green, and G. Khalil, (1993a), "Surface Pressure Field Mapping Using Luminescent Coatings," Experiments in Fluids, 14, 33-41.
17. J. Kavandi, J.B. Callis, M.P. Gouterman, G. Khalil, D. Wright, E. Green, D. Burns, and B. McLachlan, (1990), "Luminescent Barometry in Wind Tunnels," Rev. Sci. Instrum. 61(11), 3340-3347.
18. M.J. Morris, "Aerodynamic Applications of Pressure Sensitive Paint," AIAA Journal, 31 (3), March 1993, pp. 419-421.
19. T. Liu, B. Campbell, S. Burns and J. Sullivan, (1997a), "Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics," Applied Mechanics Reviews, Vol. 50, No. 4, 227-246.
20. M. E. Sellers, "Application of pressure sensitive paint for determining aerodynamic loads on a scale model of the F-16C, AIAA Paper 2000-2528, AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 21st, Denver, CO, June 19-22, 2000.
21. th Pressure Sensitive Paint Workshop, Washington, DC, 2000.
22. T.R. Amer, T. Liu and D.M. Oglesby, "Characterization of Pressure Sensitive Paint Intrusiveness Effects on Aerodynamic Data," AIAA Paper 2001-0556, AIAA, Aerospace Sciences Meeting and Exhibit, 39th, Reno, NV, Jan. 8-11, 2001.
23. T. Liu, M. Guille, and J. P. Sullivan, "Accuracy of Pressure Sensitive Paint," AIAA Paper 99-3785, AIAA Fluid Dynamics Conference, 30th, Norfolk, VA, June 28-July 1, 1999.
24. F. G. Vanhoutte, P. R. Ashill and K. P. Garry, "Intrusion Effects of Pressure Sensitive Paint in Wind-Tunnel Tests on Wings," AIAA Paper 2000-2525, AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 21st, Denver, CO, June 19-22, 2000.
25. L.N. Cattafesta III and J.G. Moore, (1995), "Uncertainty Estimates for Luminescent Temperature-Sensitive Paint Intensity Measurements," AIAA Paper 95-2193.
26. L. Cattafesta, T. Liu and J. Sullivan, (1998), "Uncertainty Estimates for Temperature Sensitive Paint Measurements with CCD Cameras," AIAA J. Vol. 36, No. 11, 2102-2108.
27. W.M. Ruyten, (1997), "Correcting Luminescent Paint Measurements for Self-Illumination," ICIASF '97 Record, International Congress on Instrumentation in Aerospace Simulation Facilities, Pacific Grove, CA, September 29-October 2, 3-9.
28. W. Ruyten and C.J. Fisher, "On the Effects of Reflected Light in Luminescent Paint Measurements," AIAA Paper 2000-0833, AIAA, Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000.
29. nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Jun 24 - 26, St. Louis, MI.
30. A.G. Davies, D. Bedwell, M. Dunleavy and N. Brownjohn, "Recent Developments in Pressure Sensitive Paint Measurements Using the BAe System, Wind tunnels and wind tunnel test techniques," Proceedings of the Conference, Cambridge, United Kingdom Apr. 14-16, 1997; London, United Kingdom, Royal Aeronautical Society, 1997, p. 28.1-28.11.
31. A.G. Davies, D. Bedwell, M. Dunleavy and N. Brownjohn, (1995), "Pressure Sensitive Paint Measurements Using a Phosphorescence Lifetime Method," presented at Seventh International Symposium on Flow Visualization, September 11-14, Seattle, Washington.
32. A.G. Davies, D. Bedwell, M. Dunleavy and N. Brownjohn, "Pressure Sensitive Paint Limitations and Solutions," ICIASF '97 - International Congress on Instrumentation in Aerospace Simulation Facilities, 17th, Pacific Grove, CA Sept. 29-Oct. 2, 1997, Record; Piscataway, NJ, Institute of Electrical and Electronics Engineers, Inc., 1997, p. 11-21.
33. R.H. Engler and C. Klein, (1997), "DLR PSP System: Intensity and Lifetime Measurements," ICIASF '97 Record, International Congress on Instrumentation in Aerospace Simulation Facilities, Pacific Grove, CA, September 29-October 2, 46-56.
34. J.W. Holmes, "Analysis of Radiometric, Lifetime and Fluorescent Lifetime Imaging for Pressure Sensitive Paint," Aeronautical Journal (0001-9240), vol. 102, no. 1014 Apr. 1998, p. 189-194.
35. K. Mitsuo, Y. Egami, K. Asai, H. Suzuki and H. Mizushima, "Development of Lifetime Imaging System for Pressure-Sensitive Paint, " AIAA Paper 2002-2909, 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
36. J.W. Holmes, "Analysis of Radiometric, Lifetime and Fluorescent Lifetime Imaging for Pressure Sensitive Paint, Wind tunnels and Wind Tunnel Test Techniques; Proceedings of the Conference, Cambridge, United Kingdom Apr. 14-16, 1997; London, United Kingdom, Royal Aeronautical Society, 1997, p. 27.1-27.8.
37. J.W. Holmes, (1998), "Analysis of Radiometric, Lifetime and Fluorescent Lifetime Imaging for Pressure Sensitive Paint, The Aeronautical Journal of the Royal Aeronautical Society, April, 189-194.
38. J.H. Bell and L.A. Hand, "The Pseudo Wind-Off Method for Intensity-Based PSP Measurements," AIAA Paper 98-0586, AIAA Aerospace Sciences Meeting & Exhibit, 36th, Reno, NV, Jan. 12-15, 1998.
39. th Pressure Sensitive Paint Workshop, Hampton, VA, 2001.
40. th Pressure Sensitive Paint Workshop, Hampton, VA, 2001.
41. th Pressure Sensitive Paint Workshop, Hampton, VA, 2001.
42. M. Hamner, B. Campbell, T. Liu, and J. Sullivan, (1994), "A Scanning Laser System for Temperature and Pressure Sensitive Paint," AIAA Paper 94-0728.
43. P. Hartmann and W. Ziegler, (1996), "Lifetime Imaging of Luminescent Oxygen Sensors Based on All-Solid-State Technology," Analytical Chemistry, 68, 4512-4514.
44. J. P. Hubner, John D. Abbitt, and B. F. Carroll, "Pressure Measurements on Rotating Machinery Using Lifetime Imaging of Pressure Sensitive Paint," AIAA Paper 96-2934, AIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 32nd, Lake Buena Vista, FL, July 1-3, 1996.
45. W.M. Baker, "Experiences with Pressure Sensitive Paint Testing," AIAA Paper 2001-0306, AIAA, Aerospace Sciences Meeting and Exhibit, 39th, Reno, NV, Jan. 8-11, 2001.
46. S.D. Torgerson, T. Liu, and J.P. Sullivan, "Use of Pressure Sensitive Paints in Low Speed Flows," AIAA Paper 96-2184, AIAA, Advanced Measurement and Ground Testing Technology Conference, 19th, New Orleans, LA, June 17-20, 1996.
47. A.E. Baron, S. Danielson, D. Paramaporn, M. Gouterman, (1995), "Evaluation of Spatial Homogeneity of Pressure Sensitive Paint Formulations," Flow Visualization VII; Proceedings of the 7th International Symposium on Flow Visualization, Seattle, WA.
48. G.A. Clinehens and G. A. Dale, (1998), "Ultrastable Blue-LED Illumination Sources for PSP Applications," Proceedings of the Sixth Annual Pressure Sensitive Paint Workshop, The Boeing Company, Seattle, Washington, October 6-8, 22-1 to 11-9.
49. G. Dale, H. Baust, C. Tyler, J. Jordan, W. Weaver and G. Clinehens, (1998), "Pressure Sensitive Paint Measurements in Very Low-Speed Flows, Proceedings of the Sixth Annual Pressure Sensitive Paint Workshop, The Boeing Company, Seattle, Washington, October 6-8, 16-1 to 16-6.
50. th International Instrumentation Symposium, May 6-10, 2001, Denver, CO; published in Conference Proceedings (Instrument Society of America, Research Triangle Park, NC, 2001).
51. J. Crafton, N. Lachendro, M. Guille, J.P. Sullivan, and J.D. Jordan, "Application of Temperature and Pressure Sensitive Paint to an Obliquely Impinging Jet," AIAA Paper 99-0387, AIAA, Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan. 11-14, 1999.
52. Y. Shimbo, K. Asai, H. Kanda, Y. Iijima, N. Komatsu, S. Kita, and M. Ishiguro, "Evaluation of Several Calibration Techniques for Pressure Sensitive Paint in Transonic Testing," AIAA Paper 98-2502, AIAA, Advanced Measurement and Ground Testing Technology Conference, 20th, Albuquerque, NM, June 15-18, 1998.
53. Bradley, L. C. (1995), "A Temperature-Sensitive Phosphor Used to Measure Surface Temperature in Aerodynamics," Review of Scientific Instruments 24(3), 219-220.
54. A. Bykov, S. Fonov, V. Mosharov, A. Orlov, V. Pesetsky, and V. Radchenko, V. (1997), "Study Result for the Application of Two-Component PSP Technology to Aerodynamic Experiment," AGARD Conference Proceedings CP-601, Advanced Aerodynamic Measurement Technology, 29-1 to 29-8.
55. J. Harris and M. Gouterman, (1995), "Referenced Pressure Sensitive Paint," Flow Visualization VII, Proceeding of the Seventh International Symposium on Flow Visualization, edited by J. Crowder, Seattle, Washington, p.802.
56. J.D. Jordan, A.N. Watkins, W.L. Weaver, G.A. Dale and K.R. Navarra, "Sol-Gel-Based Pressure-Sensitive Paint Development," AIAA Paper 99-0566, Reno, NV.
57. M. Lyonnet, "The Two-Component PSP Investigation On a Civil Aircraft Model in S2MA Wind Tunnel," Pressure-Sensitive Paint ONERA, TP no. 1997-101, Pressure Sensitive Paint Workshop, 5th, Arnold AFB, TN May 14-16, 1997.
58. D.M. Oglesby, B.D. Leighty and B.T. Upchurch, (1995), "Pressure Sensitive Paint with an Internal Reference Luminophore," Proceedings of the 41st International Instrumentation Symposium, Instrument Society of America, Denver, CO, 381-395.
59. D.M. Oglesby, B.T. Upchurch, B.D. Leighty and K.A. Simmons, (1996), "Pressure Sensitive Paint With Internal Temperature Sensing Luminophore," Proceedings of the 42nd International Instrumentation Symposium, Instrument Society of America, San Diego, CA.
60. D.M. Oglesby, J.P. West, B.T. Upchurch and B.D. Leighty, "Pressure Sensitive Paint with Internal Correction for Light and Temperature," International Instrumentation Symposium, 44th, Reno, NV May 3-7, 1998, Proceedings; Research Triangle Park, NC, Instrument Society of America, 1998, p. 591-603.
61. K.S. Schanze, B.F. Carroll, S. Korotkevitch and M. Morris, (1997), "Temperature Dependence of Pressure Sensitive Paints," AIAA J., Vol. 35, No. 2, February, 306-310.
62. K.S. Schanze, B.F. Carroll, S. Korotkevitch and M. Morris, (1997), "Concerning the Temperature Dependence of Pressure Sensitive Paints," AIAA Paper 97-0386.
63. M.A. Woodmansee and J.C. Dutton, "Treating Temperature-Sensitivity Effects of Pressure-Sensitive Paint Measurements," Experiments in Fluids (0723-4864), vol. 24, no. 2 Feb. 1998, p. 163-174.
64. E. Puklin, "Fluoroacrylic Polymer for Luminescent Pressure Sensitive Paint (PSP)," M.S. Thesis, University of Washington, 1999.
65. US Patent Application No. 09/558,722. "Temperature Independent Pressure Sensitive Paints," filed April 26, 2000.
66. A. Bykov, S. Fonov, V. Mosharov, A. Orlov, V. Pesetsky, and V. Radchenko, (1997), "Study Result for the Application of Two-Component PSP Technology to Aerodynamic Experiment," AGARD Conference Proceedings CP-601, Advanced Aerodynamic Measurement Technology, 29-1 to 29-8.
67. M. Lyonnet, B. Deleglise, G. Grenat, A. Bykov, V. Mosharov, A. Orlov, and S. Fonov, "The Two Component PSP Investigation on a Civil Aircraft Model in S2MA Wind Tunnel," AGARD Proceedings, Seattle, WA, 1997.
68. th Australasian Fluid Mechanics Conference, Monash University, Melbourne, Australia, 1998.
69. th Pressure Sensitive Paint Workshop, Hampton, VA, 2000.
70. th Pressure Sensitive Paint Workshop, Washington, DC, 2001.
71. th Pressure Sensitive Paint Workshop, Washington, DC, 2002.
72. D.M. Oglesby, B.T. Upchurch, B.D. Leighty and K.A. Simmons, (1996), "Pressure Sensitive Paint With Internal Temperature Sensing Luminophore," Proceedings of the 42nd International Instrumentation Symposium, Instrument Society of America, San Diego, CA.
73. th International Instrumentation Symposium, Reno, NV May 3-7, 1998, Proceedings; Research Triangle Park, NC, Instrument Society of America, 1998, p. 591-603.
74. th International Instrumentation Symposium, May 6 - 10, 2001, Denver, CO; published in Conference Proceedings (Instrument Society of America, Research Triangle Park, NC, 2001).
75. th International Instrumentation Symposium, May 6 - 10, 2001, Denver, CO; published in Conference Proceedings (Instrument Society of America, Research Triangle Park, NC, 2001).
76. th International Instrumentation Symposium, April 30 - May 4 2000, Bellevue, WA; published in Conference Proceedings (Instrument Society of America, Research Triangle Park, NC, 2000).
77. th Pressure Sensitive Paint Workshop, Hampton, VA, 2001.
78. th Pressure Sensitive Paint Workshop, Washington, DC, 2002.
79. nd AMT Conference, St. Louis, MO, June 24 - 27, 2002.
80. E. Puklin, B. Carlson, S. Gouin, C. Costin, E. Green, S. Ponomarev, H. Tanji and M. Gouterman, (1998), "Ideal Pressure Sensitive Paint: PtTFPP in FIB polymer," Proceedings of the Sixth Annual Pressure Sensitive Paint Workshop, The Boeing Company, Seattle, Washington, October 6-8, 8-1 to 8-22.
81. J. Harris and M. Gouterman, (1995), "Referenced Pressure Sensitive Paint," Flow Visualization VII, Proceeding of the Seventh International Symposium on Flow Visualization, edited by J. Crowder, Seattle, Washington, p.802.
82. J. Harris and M. Gouterman, (1998), "Referenced Pressure Sensitive Paint Using Blue Emitting Phosphors," Proceeding of the Sixth Annual Pressure Sensitive Paint Workshop, The Boeing Company, Seattle, WA, 6-8, 19-1 to 19-13.
83. D. McLean, (1998), "Referenced Pressure Paint and the Ratio-of-Ratios," Proceedings of the Sixth Annual Pressure Sensitive Paint Workshop, The Boeing Company, Seattle, WA.
84. J. Harris and M. Gouterman, "Referenced Pressure Sensitive Paint," Flow Visualization VII; Proceedings of the 7th International Symposium on Flow Visualization, Seattle, WA.
85. th International Instrumentation Symposium, April 30 - May 4 2000, Bellevue, WA; published in Conference Proceedings (Instrument Society of America, Research Triangle Park, NC, 2000).
86. J.F. Donovan, M.J. Morris, A. Pal, M.E. Benne and R.C. Crites, (1993), "Data Analysis Techniques for Pressure- and Temperature-Sensitive Paint," AIAA Paper 93-0176.
87. Y.I. Abdel-Aziz and H.M. Karara, (1971), "Direct Linear Transformation from Comparator Coordinates Into Object Space Coordinates in Close-Range Photogrammetry," Proc. ASP/UI Symp. On Close-Range Photogrammetry, Univ. of Illinois at Urbana-Champaign, Urbana, Illinois, 1-18.
88. Y. Le Sant, B. Deleglise and Y. Mebarki, "An Automatic Image Alignment Method Applied to Pressure Sensitive Paint Measurements," ONERA, TP no. 1997-162, ICIASF '97 - International Congress on Instrumentation in Aerospace Simulation Facilities, 17th, Pacific Grove, CA Sept. 29-Oct. 2, 1997, Record; Piscataway, NJ, Institute of Electrical and Electronics Engineers, Inc., 1997, p. 57-65.
89. th International Symposium on Flow Visualization, Seattle, WA Sept. 11-14, 1995; New York, Begell House, Inc., 1995, p. 812-817.
90. W.L. Weaver, J.D. Jordan, G.A. Dale and K.R. Navarra, (1999), "Data Analysis Methods for the Development and Deployment of Pressure Sensitive Paints," AIAA Paper 99-0565.
91. Y,I. Abdel-Aziz and H.M. Karara, (1971), "Direct Linear Transformation From Comparator Coordinates into Object Space Coordinates in Close-Range Photogrammetry," Proc. ASP/UI Symp. On Close-Range Photogrammetry, Univ. of Illinois at Urbana-Champaign, Urbana, Illinois, 1-18.
92. M.M. Ardasheva, L.B. Nevsky and G.E. Pervushin, "Method of Pressure Distribution Measurement with the Indicating Coating," J. App. Mech. & Tech. Phys. 26(4), 469-474, 1985.
93. A. Andreev, A. Bukov, M. Ipatov, S. Kabin, P. Nushtaev, A. Orlov, V. Mosharov, V. Radchenko, V. Pestsly and S. Fonov, "Pressure Field Investigation by LPS Technology on the Aerospacecraft Model Buran in the TsAGI Wind Tunnel T-112," Preprint No. 75, TsAGI, Moscow, 1993.
94. A.O. Andreev, A.P. Bykov, W.M. Ipatov, S.V. Kabin, P.D. Nushtaev, A.A. Orlov, P.E Mosharov, V.N. Radchenko, V.A. Pesetsky and S.D. Fonov, "Pressure Fields Investigation by LPS Technology on the Aerospacecraft Model," J. Phys. III France 4 (1994) 2317-2337.
95. J.H. Bell and B.G. McLachlan, "Image Registration for Pressure-Sensitive Paint Applications," Experiments in Fluids, vol. 22, no. 1, p. 78-86 November 1996.
96. J.H. Bell and B.G. McLachlan, (1993), "Image Registration for Luminescent Paint Sensors," AIAA Paper 93-0178.
97. th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF), Monterey, CA, 1997.
98. W. Ruyten, "Toward an Integrated Optical Data System for Wind Tunnel Testing," AIAA Paper 99-0181, AIAA, Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan. 11-14, 1999.
99. J. Lepicovsky, T.J. Bencic and R.J., "Application of Pressure Sensitive Paint to Confined Flow at Mach Number 2.5," AIAA Paper 97-3214, AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 33rd, Seattle, WA, July 6-9, 1997.
100. W. Ruyten, "Model Attitude Measurement with an Eight-Camera Pressure-Sensitive Paint System," AIAA Paper 2000-0831, AIAA Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000.
101. T.J. Bencic, "Rotating Pressure and Temperature Measurements on Scale-Model Fans Using Luminescent Paints," AIAA Paper 98-3452, AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 34th, Cleveland, OH, July 13-15, 1998.
102. T.J. Bencic, "Calibration of Detection Angle for Full Field Pressure-Sensitive Paint Measurements," AIAA Paper 2001-0307, AIAA, Aerospace Sciences Meeting and Exhibit, 39th, Reno, NV, Jan. 8-11, 2001.
103. T.J. Bencic, "Development of Advanced Optical Instrumentation for Use in the NASA Glenn Icing Research Tunnel," AIAA Paper 2001-0396, AIAA, Aerospace Sciences Meeting and Exhibit, 39th, Reno, NV, Jan. 9-11, 2001.
104. T.J. Bencic, "Application of Pressure Sensitive Paint to Ice Accreted Wind Tunnel Models," AIAA Paper 2000-0834, AIAA, Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000.
105. M. Lyonnet, B. Deleglise and Y. Lesant, "Application of Pressure Sensitive Paint Technique in the S1MA ONERA Wind Tunnel," AIAA Paper 2002-0744, AIAA Aerospace Sciences Meeting & Exhibit, 40th, Reno, NV, Jan. 14-17, 2002.
106. Y. Le Sant, F. Bouvier, M.-C. Merienne and J.-L. Peron, "Speed tests using PSP at ONERA," AIAA Paper 2001-0555, AIAA, Aerospace Sciences Meeting and Exhibit, 39th, Reno, NV, Jan. 8-11, 2001.
107. E.T. Schairer and L.A. Hand, (1997), "Pressure-Sensitive Paint Measurements on Aeroelastic Wings in Transonic Flow," AIAA Paper 97-0389.
108. S. Fonov, V. Mosharov, V. Radchenko, R. Engler and C. Klein, "Application of the PSP for Investigation of the Oscillating Pressure Fields," AIAA-98-2503, Albuquerque, NM.
109. th International Instrumentation Symposium.
110. J.D. Jordan, A.N. Watkins, W.L. Weaver, G.A. Dale and K.R. Navarra, (1999), "Sol-Gel-Based Pressure Sensitive Paint Development," AIAA Paper 99-0566.
111. B.F. Carroll, J.D. Abbitt, E.W. Lukas and M.J. Morris, (1996), "Step Response of Pressure Sensitive Paints," AIAA J, Vol. 34, No. 3, 521-526.
112. M. Matsumoto, G. Masuya, S. Tomioka, Y. Ikeda and S. Teramoto, "PSP Measurement of Fuel Mixing in a Supersonic Combustor of Scram-Jet Engine Model," AIAA Paper 2002-0235, AIAA Aerospace Sciences Meeting & Exhibit, 40th, Reno, NV, Jan. 14-17, 2002.
113. Y. Sakamura, T. Suzuki, M. Matsumoto and Y. Ikeda, "Optical Measurements of High-Frequency Pressure Fluctuations Using PSP and Cassegrain Optics,' AIAA Paper 2002-0537, AIAA Aerospace Sciences Meeting & Exhibit, 40th, Reno, NV, Jan. 14-17, 2002.
114. B.F. Carroll, A. Winslow, J. Abbitt, K. Schanze and M. Morris, (1995), "Pressure Sensitive Paint: Application to a Sinusoidal Pressure Fluctuation," ICIASF '95 Record, International Congress on Instrumentation in Aerospace Simulation Facilities, Wright-Patterson Air Force Base, Dayton, OH, USA, 35.1-35.6.
115. B.E. Carroll, J.D. Abbitt, E.W. Likas and M.J. Morris, (1995), "Step Response of Pressure-Sensitive Paints," AIAA Paper 95-0483.
116. N.A. Winslow, B.F. Carroll and F.M. Setzer, (1996), "Frequency Response of Pressure Sensitive Paints," AIAA Paper 96-1967.
117. K. Asai, H. Kanda, T. Kunimasu, T. Liu and J. Sullivan, (1996), "Detection of Boundary-Layer Transition in a Cryogenic Wind Tunnel by Using Luminescent Paint," AIAA Paper 96-2185.
118. K. Asai, T. Kunimasu and Y. Iijima, "Visualization of the Quiet Test Region in a Supersonic Wind Tunnel Using Luminescent Paint," 17th International Congress on Instrumentation in Aerospace Simulation Facilities Sep 29-Oct 2, 1997.
119. th Pressure Sensitive Paint Workshop, Washington, DC.
120. H. Sakaue, S. Matsumura, S. Schneider and J. Sullivan, "Anodized Aluminum Pressure Sensitive Paint for Short Duration Testing," AIAA Paper 2002-2908, 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
121. K. Nakakita and K. Asai, "Pressure Sensitive Paint Application to a Wing-Body Model in a Hypersonic Shock Tunnel," AIAA Paper 2002-2911, 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
122. K. Nakakita, T. Yamazaki, K. Asai, N. Teduka, A. Fuji and M. Kameda, "Pressure Sensitive Paint Measurement in a Hypersonic Shock Tunnel," AIAA Paper 2000-2523, AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 21st, Denver, CO, June 19-22, 2000.
123. H. Sakaue, J.W. Gregory, J.P. Sullivan and S. Raghu, "Pressure Sensitive Paint for Unsteady Flow Fields," AIAA Paper 2001-0554, AIAA, Aerospace Sciences Meeting and Exhibit, 39th, Reno, NV, Jan. 8-11, 2001.
124. Y. Shimbo, M. Noguchi and Y. Makino, "Blowdown Tunnel Application of Pressure Sensitive Paint," AIAA Paper 99-3169, AIAA Applied Aerodynamics Conference, 17th, Norfolk, VA, June 28-July 1, 1999, Collection of Technical Papers (A99-33352 08-02).
125. Y. Shimbo, R.D. Mehta and B.J. Cantwell, "Vortical Flow Field Investigation Using the Pressure Sensitive Paint Technique at Low Speed," AIAA Paper 97-0388, AIAA Aerospace Sciences Meeting & Exhibit, 35th, Reno, NV, Jan. 6-9, 1997.
126. F. Drouillard II, C.W. Fisher, M.A. Linne, N.T. Middleton, G.J. Fiechtner, L.P. Goss and J.R. Gord, "Evaluation of New Camera Architectures for Pressure Sensitive Paint Measurements," AIAA Paper 2000-2524 (AIAA Accession number 33565), AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 21st, Denver, CO, June 19-22, 2000.
127. J.R. Lakowicz, Principles of Fluorescence Spectroscopy, Plenum Press, New York, NY, 1983.
128. http://www.roperscientific.com
129. http://www.innssi.com