Pressure-sensitive paint measurements in a blowdown wind tunnel

Journal of Aircraft

Volumn 42, Issue 4, 2005, Pages 908-915

  Raju, Channa ^a,b   Viswanath, P R ^b  

^a SURFACE ENGINEERING DIVISION   (India)

^b Experimental Aerodynamics Division   (India)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; PRESSURE EFFECTS; PRESSURE MEASUREMENT; TEMPERATURE CONTROL; THERMOCOUPLES; TUNNELS;

AIRCRAFT MODEL; MEAN MODEL TEMPERATURE; PRESSURE TAPS; PRESSURE-SENSITIVE PAINT;

WIND TUNNELS;

EID: 24144475034     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.7224     Document Type: Article

References (18)

1. Sellers, M. E., "Application of Pressure Sensitive Paint for Determining Aerodynamic Loads on a Scale of the F-16C," AIAA Paper 2000-2528, June 2000.
2. Engler, R. H., Klein, C., Merlo, E., and Amerom, P. V., "360° PSP Measurements in Transonic Flow," Proceedings 16th International Congress on Instrumentation in Aerospace Simulation Facilities, IEEE, Cleveland, 2001.
3. Schairer, E. T., Mehta, R. D., and Olsen, M. E., "Effects of Pressure-Sensitive Paint on Experimentally Measured Wing Forces and Pressures," AIAA Journal, Vol. 40, No. 9, 2002, pp. 1830-1838.
4. Crites, R. C., "Pressure Sensitive Paint Technique," Measurement Techniques, Lecture Series 1993-05, Von Karman Institute of Fluid Dynamics, Rhode Saint Genese, Belgium, 1993.
5. Liu, T., Campbell, B. T., Bums, S. P., and Sullivan, J. P., "Temperature and Pressure Sensitive Luminescent Paints in Aerodynamics," Applied Mechanics Reviews, Vol. 50, No. 4, 1997, pp. 227-246.
6. Bell, J. H., Schairer, E. T., Hand, L. A., and Mehta, R. D., "Surface Pressure Measurements Using Luminescent Coatings," Annual Review of Fluid Mechanics, Vol. 33, Jan. 2001, pp. 155-206.
7. Liu, T., Guille, M., and Sullivan, J. P., "Accuracy of Pressure Sensitive Paint," AIAA Paper 99-3785, June-July 1999.
8. Woodmansee, M. A., and Dutton, J. C., "Treating Temperature- Sensitivity Effects of Pressure Sensitive Paint Measurements," Experiments in Fluids, Vol. 24, No. 2, 1998, pp. 163-174.
9. Shimbo, Y., Noguchi, M., and Makino, Y., "Slowdown Tunnel Application of Pressure Sensitive Paint," AIAA Paper 99-3169, 1999.
10. Mébarki, Y., and Le Sant, Y., "Pressure Sensitive Paint Evaluation on a Supercritical Wing at Cruise Speed," Journal of Visualization, Vol. 4, No. 4, 2001, pp. 313-322.
11. Egami, Y., Iijima, Y., Amao, Y., Asai, K., Fuji, A., Teduka, N., and Kameda, M., "Quantitative Visualisation of the Leading-edge Vortices on a Delta Wing by Using Pressure Sensitive Paint," Journal of Visualization, Vol. 4, No. 2, 2001, pp. 139-150.
12. Mitsuo, K., Asai, K., Hayasaka, M., and Kameda, M., "Temperature Correction of PSP Measurement Using Dual-Luminophor Coating," Journal of Visualization, Vol. 6, No. 3, 2003, pp. 213-223.
13. Klein, C., Engler, R. H., Raju, C., Viswanath, P. R., and Achar, S. P. J., "PSP Measurements on a Wing-Body Model in the 1.2 m Trisonic Wind Tunnel," NAL Report NAL-SP-0110, Experimental Aerodynamics Division, National Aerospace Laboratories, Bangalore, Aug. 2001.
14. Kline, S. J., and McClintock, F. A., "Describing Uncertainties in Single-Sample Experiments," Mechanical Engineering, Vol. 75, Jan. 1953, pp. 3-8.
15. Venkatakrishnan, L., "Application of Resection on PSP Data Processing," NAL Report NAL-PD-3114, Experimental Aerodynamics Division, National Aerospace Laboratories, Bangalore, Nov. 2003.
16. Liu, T., Cattafesta, L. N., and Radeztsky, R. H., "Photogrammetry Applied to Wind Tunnel Testing," AIAA Journal, Vol. 38, No. 6, 2000, pp. 964-971.
17. Mendoza, D. R., "An Analysis of CCD Camera Noise and Its Effect on Pressure Sensitive Paint Instrumentation System Signal to Noise Ratio," ICIASF '97 IEEE, Pacific Grove, CA, 1997, pp. 22-29.
18. Dowgwillo, R. M., Morris, M. J., Donovan, J. F., and Benne, M. E., "Pressure Sensitive Paint in Transonic Wind-Tunnel Testing of the F-15," Journal of Aircraft, Vol. 33, No. 1, 1996, pp. 109-116.