Luminescent Paints for Pressure and Temperature Measurements

  • James H. Bell
  • Timothy J. Bencic


Designers in a variety of fields require knowledge about temperature and pressure distributions across surfaces, but this requirement is especially acute for aerospace engineers. Detailed knowledge about pressure distributions, transition between laminar and turbulent flows, cooling flow properties, and more make the difference between successful and unsuccessful aircraft and spacecraft. For decades, test engineers have instrumented wind tunnel models with discrete, electronic pressure transducers and thermocouples to make as many measurements as they could afford. Aircraft design programs require models with many hundreds of individual pressure taps; engine design programs require similar numbers of thermocouples. Highly instrumented models can take skilled laborers months to prepare, yielding high costs for these data. Yet the costs are paid because of the criticality of the measurements.


Wind Tunnel Shot Noise 40th AIAA Aerospace Optical Metrology Luminescent Paint 
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  1. 1.
    Pervushin, G.E., Nevsky, L.B. 1981 “Composition for indicating coating” USSR patent SU 1065452 A.Google Scholar
  2. 2.
    Ardasheva, M.M., Nevsky, L.B., Pervushin, G.E. 1982 “Method of pressure distribution visualization with the organic luminophores” III the USSR School on the methods of aerophysical investigations pp. 103–107 (in Russian).Google Scholar
  3. 3.
    Ardasheva, MM, Nevsky, L.B., Pervushin, G.E. 1985 “Method of pressure distribution measurement with the indicating coating” J. App. Mech. & Tech. Phys. (PMTF) 26(4) pp. 469–474 (in Russian).ADSCrossRefGoogle Scholar
  4. 4.
    Mosharov, V., Radchenko, V., Fonov, S. 1997 “Luminescent pressure sensors in aerodynamic experiment”, pub. Central Aerohydrodynamic Institute (TsAGI) CWA International Corporation. Google Scholar
  5. 5.
    Radchenko, V.E. 1985 “Application of the luminescence in aerodynamic researches” Master ‘s thesis, Moscow Physical-Technical Institute, Zhukovsky (in Russian).Google Scholar
  6. 6.
    Gouterman, M., Kavandi, J., Gallery, J., Callis, J. 1990 “Surface pressure measurement by oxygen quenching of luminescence” US 5186046, EP 0472243 A2.Google Scholar
  7. 7.
    Kavandi, J.L., Callis, J.C., Gouterman, M., Khalil, G., Wright, D., Green, E., Burns, D., McLachlan, B.G. 1990 “Luminescent barometry in wind tunnels” Rev. Sci. Inst., 61(11) Nov pp. 3340–3347. ADSCrossRefGoogle Scholar
  8. 8.
    McLachlan, B.G., Kavandi, J.L., Callis, J.B., Gouterman, M., Green, E., Khalil, G. 1990 “Surface pressure field mapping using luminescent coatings” Experiments in Fluids 14, 33–41 June. ADSGoogle Scholar
  9. 9.
    Oglesby, D.M., Puram, CK., Upchurch, B.T. 1995 “Optimization of measurements with pressure sensitive paints” NASA TM4695 June 1995. Google Scholar
  10. 10.
    Morris, M.J., Donovan, J.F., Pal, A., Benne, M.E., Crites, R.C. 1993 “Aerodynamic measurements based on photoluminescence” AIAA 93–0175 AIAA 31st Aerospace Sciences Meeting, Reno NV, January 11, 1993. Google Scholar
  11. 11.
    Sajben, M. 1993 “Uncertainty estimates for pressure sensitive paint measurements” AIAA Journal Vol. 31, No. 11 pp. 2105–2110 Nov 1993. ADSCrossRefGoogle Scholar
  12. 12.
    Sullivan, J. 2001 “Temperature and pressure sensitive paint” von Karman Institute for Fluid Dynamics Lecture Series 2001–01 Advanced Measurement Techniques Jan 29–31. Google Scholar
  13. 13.
    Brown, O. 2000 “Low-speed pressure measurements using a luminescent coating system” Ph.D. Dissertation, Stanford University. Google Scholar
  14. 14.
    Campbell, B.T., Liu, T., Sullivan, J.P. “Temperature measurement using fluorescent molecules” 1992 6th International Symposium on Application of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, July 1992.Google Scholar
  15. 15.
    Kolodner, P., Tyson, A. 1983 “Non-contact surface temperature measurement during reactive-ion etching using fluorescent polymer films” Appl. Phys. Lett. Vol. 42, no. 8, pp. 749–751. ADSCrossRefGoogle Scholar
  16. 16.
    Asai, K., Kanda, H., Kunimasu, T., Liu, T., Sullivan, J.P. 1997 “Boundary-layer transition detection in a cryogenic wind tunnel using luminescent paint” Jnl. of Aircraft vol. 34 no. 1 pp. 34–42. CrossRefGoogle Scholar
  17. 17.
    Popernack, J.R., Thomas, G., Owens, L.R., Hammer, M.P., Morris, M.J. 1997 “Application of temperature sensitive paint for detection of boundary layer transition” Proceedings of the 17 th International Congress on Instrumentation in Aerospace Simulation Facilities, Monterey California Sept. 29 1997 pp. 77–83. Google Scholar
  18. 18.
    Shimbo, Y., Asai, K., Kanda, H., Iijima, Y. 1998 “Evaluation of several calibration techniques for pressure sensitive paint in transonic testing” AIAA 98–2502 AIAA 20th Adv. Measurement and Ground Testing Technology Conf, Albuquerque New Mexico, June 15–18. Google Scholar
  19. 19.
    Woodmansee, M.A., Dutton, J.C. 1998 “Treating temperature-sensitivity effects of pressure-sensitive paint measurements” Experiments in Fluids 24, pp. 163–174 Jan. ADSCrossRefGoogle Scholar
  20. 20.
    Bell, J.H., McLachlan, B.G. 1996 “Image registration for pressure sensitive paint applications” Experiments in Fluids 22, 78–86 Jan. ADSCrossRefGoogle Scholar
  21. 21.
    Lyonnet, M., Deleglise, B., Lésant, Y. 2002 “Application of pressure sensitive paint technique in the S IMA ONERA win tunnel” AIAA-2002–0744 40 th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 14–17. Google Scholar
  22. 22.
    Holmes, J.W. 1997 “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, London, United Kingdom, Royal Aeronautical Society, p. 27.1–27.8. Google Scholar
  23. 23.
    Holmes, J.W. 1998 “Analysis of radiometric, lifetime and fluorescent lifetime imaging for pressure sensitive paint” Aero. Journal (0001–9240), vol. 102, no. 1014, Apr. p. 189–194. Google Scholar
  24. 24.
    Davies, A.G., Bedwell, D., Dunleavy, M., Brownjohn, N. 1997 “Recent developments in pressure sensitive paint using the BAe system” Wind tunnels and wind tunnel test techniques; Proceedings of the Conference, Cambridge, United Kingdom, Apr. 14–16, London, United Kingdom, Royal Aeronautical Society, p. 28.1–28.11. Google Scholar
  25. 25.
    Sellers, M.E. 2000 “Application of pressure sensitive paint for determining aerodynamic loads on a scale model of the F-16C” AIAA 2000–2528 21st AIAA Aerodynamic Measurement Technology and Ground testing Conference, Denver, CO, June 19–22. Google Scholar
  26. 26.
    Kammeyer, M., Donovan, J., Kelble, C, Benne, M.E., Kihlken, T., Felter, J.A. 2002 “Accuracy assessment of a pressure-sensitive paint measurement system” AIAA 2002–0530 40 th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 14–17. Google Scholar
  27. 27.
    Liu, T., Campbell, B., Burns, S.P., Sullivan, J.P. 1997 “Temperature- and pressure -sensitive paints in aerodynamics” Applied Mechanics Review vol. 50, no. 4 April 1997. Google Scholar
  28. 28.
    Bell, J.H., Schairer, E.T., Hand, L.A., Mehta, R.D. 2001 “Surface pressure measurements using luminescent coatings” Ann. Rev. Fluid. Mech. 33:155–206. ADSCrossRefGoogle Scholar
  29. 29.
    Schanze, K.S., Carroll, B.F., Korotkevitch, S., Morris, M.J. 1997 “Temperature dependence of pressure-sensitive paints” AIAA Jnl. vol. 35, pp. 306–10. ADSCrossRefGoogle Scholar
  30. 30.
    Gouin, S., Gouterman, M. 2000a “Ideality of pressure-sensitive paint. II Effect of annealing on the temperature-dependence of the luminescence” J. Appl. Polym. Sci. vol. 77, pp. 2805–14. CrossRefGoogle Scholar
  31. 31.
    Puklin, E., Carlson, B., Gouin, S., Costin, C, Green, E., Ponomarev, S., Tanji, H., Gouterman, M., 2000 “Ideality of pressure-sensitive paint. I. platinum tetra (pentafluorophenyl)porphine in fluoroacrylic polymer”, J. Appl. Polym. Sci., vol. 77, pp. 2795–2804. CrossRefGoogle Scholar
  32. 32.
    Schairer, E.T. 2002 “Optimum thickness of pressure-sensitive paint for unsteady measurements” AIAA Jnl. vol. 40, no. 11. Nov.pp. 2312–18. ADSCrossRefGoogle Scholar
  33. 33.
    Asai, K., Amao, Y., Iijima, Y., Okura, L, Nishide, I. 2002 “Novel pressure-sensitive paint for cryogenic and unsteady wind-tunnel testing” Jnl. of Thermophysics and Heat Transfer vol. 16, no. 1, Jan-March, pp. 109–115. CrossRefGoogle Scholar
  34. 34.
    Sakaue, H., Sullivan, J.P. 2000 “Fast response time characteristics of anodized aluminum pressure sensitive paint” AIAA 2000–0506 38 th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 10–13. Google Scholar
  35. 35.
    Goss, L.P., Trump, D.D., Sarka, B., Lydick, L.N., Baker, W.M. 2000 “Multidimensional time-resolved pressure-sensitive-paint techniques — A numerical and experimental comparison” AIAA 2000–0832 38 th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 10–13,Google Scholar
  36. 36.
    McLachlan, B.G., Bell, J.H., Park, H., Kennelly, R.A., Schreiner JA, Smith SC, Strong JM, Gallery J, Gouterman M. 1995 “Pressure-sensitive paint measurements on a supersonic high-sweep oblique wing model” AIAA Jnl. of Aircraft, vol. 32, no. 2, Mar-Apr, pp.217–227.CrossRefGoogle Scholar
  37. 37.
    Dale, G.A., Gaust, H.D., Clinehans, G.A. 1999 “Implementing pressure-sensitive paint in the AFRL subsonic aerodynamic research laboratory” Proceedings of the 18 th International Congress on Inst, in Aerospace Sim. Facilities, Toulouse, France June 14–17 pp. 20.1–8. Google Scholar
  38. 38.
    Guille, M., Sullivan, J.P., Holmes, J. 1999 “Comparison of luminescent paints measurement systems” Proceedings of the 18 th International Congress on Instrumentation in Aerospace Simulation Facilities, Toulouse, France June 14–17 pp. 16.1–10. Google Scholar
  39. 39.
    Ingram, J., Oglesby, D. 2002 “Solving pressure sensitive paint challenges using chemistry” presentation at 9 th Pressure-Sensitive Paint Workshop, Washington B.C. April 7–11. Google Scholar
  40. 40.
    Nishide, H. 2002 “Metalloporphyrin polymer coatings for oxygen pressure measurement” Proceedings of the 2 nd International Conference on Porphyrins and Phthalocyanines, Kyoto, Japan, June 30 — July 5. Google Scholar
  41. 41.
    Hollerman, W.A., Allison, S.W., Beshears, D.L., Guidry, R.F., Bencic, T.J., Mercer, CR., Eldridge, J.I., Cates, M.R., Boudreaux, P., Goedeke, S.M., 2002, “Development of Fluorescent Coatings for High Temperature Aerospace Applications”, Proceedings of the 2002 Core Technologies for Space Systems Conference, Colorado Springs, CO., November 19–21,2002.Google Scholar
  42. 42.
    Mikhail, E.M., Bethel, J.S., McGlone, J.C. 2001 “Introduction to modern photogrammetry”, John Wiley & Sons, New York, NY. Google Scholar
  43. 43.
    Abdel-Aziz, Y., Karara, H. 1971 “Direct linear transformation from comparator coordinates into object space coordinates” Proc. ASP/UI Symp. On Close-Range Photogrammetric Systems, Urbana, Illinois, pp. 1–48. Google Scholar
  44. 44.
    Bell, J.H., Schairer, E.T. 2002 “Texture mapping for display and analysis of image data on 3d surfaces”, AIAA-2002–0745 40 th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 14–17. Google Scholar
  45. 45.
    Zaman, K.B., Dahl, M.D., Bencic, T.J., Loh, C.Y., 2002, “Investigation of a ‘transonic resonance’ with convergent-divergent nozzles”, J. Fluid Mech. vol. 463, pp. 313–343. MathSciNetADSzbMATHCrossRefGoogle Scholar

Copyright information

© Springer Science+Business Media New York 2003

Authors and Affiliations

  • James H. Bell
    • 1
  • Timothy J. Bencic
    • 2
  1. 1.Ames Research CenterNational Aeronautics and Space AdministrationUSA
  2. 2.Glenn Research CenterNational Aeronautics and Space AdministrationUSA

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