Pressure-sensitive paint technology applied to low-speed automotive testing

SAE Technical Papers

Volumn , Issue , 2001, Pages

  Duell, Edward ^a   Everstine, Douglas ^b   Mehta, Rabindra ^c   Bell, James ^c   Perry, Mark ^d  

^a JACOBS TECHNOLOGY   (United States)

^b FORD MOTOR COMPANY   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

^d Lockheed Martin Low Speed Wind Tunnel   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCEPTANCE TESTS; LUMINOUS PAINT; PAINT; PRESSURE DISTRIBUTION; SIGNAL TO NOISE RATIO; SUPERSONIC AERODYNAMICS; WIND STRESS;

AUTOMOTIVE WIND TUNNELS; BACKWARD FACING STEP; HIGH DYNAMIC PRESSURE; PRESSURE COEFFICIENTS; PRESSURE SENSITIVE PAINTS; QUANTITATIVE ACCURACY; QUANTITATIVE PRESSURES; QUANTITATIVE RESULT;

WIND TUNNELS;

EID: 85072458305     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2001-01-0626     Document Type: Conference Paper

References (17)

1. McLachlan, B.G., Bell, J.H., "Pressure-Sensitive Paint in Aerodynamic Testing" Exp. Thermal Fluid Sci. 10: 475-480, 1995.
2. Liu, T., Campbell, B.T., Burns, S.P., Sullivan, J.P., "Temperature and Pressure Sensitive Luminescent Paints in Aerodynamics" App. Mech. Rev., 50 (4): 227-246, 1997.
3. Brown, O., Mehta, R.D., Cantwell, B.J., "Low-Speed Flow Studies Using the Pressure Sensitive Paint Measurement Technique" AGARD-CP-601, pp. 31-1-31-13, May 1998. Also presented at AGARD 81st Fluid Dynamics Panel Symposium on Advanced Aerodynamic Measurement Techniques, Seattle, WA, Sept. 22-25, 1997.
4. Brown, O.C., "Low-Speed Pressure Measurements Using a Luminescent Coating System" PhD thesis, Stanford University, 2000. (Also, Joint Institute of Aeronautics and Astronautics Tech. Rep. 123, May, 2000, Stanford University).
5. Morris, M.J., Benne, M.E., Crites, R.C., Donovan, J.F., "Aerodynamic Measurements Based on Photoluminescence" AIAA Paper 93-0175, 31st Aerospace Sciences Meeting, Reno, NV, 1993.
6. Crites, R., Benne, M., "Emerging Technology for Pressure Measurement in Wind Tunnels-Pressure Sensitive Paint" AIAA Paper 95-0106, 1995.
7. Bell, J.H., McLachlan, B.G., "Image Registration for Pressure-Sensitive Paint Applications" Experiments in Fluids, 22, pp 78-86, 1996.
8. Bell, James H., Hand, L. A., "The Pseudo Wind-off Method for Intensity-Based PSP Measurements" AIAA Paper 98-0568, 36th Aerospace Sciences Meeting, Reno, NV, 1998.
9. Fonov, S., Mosharov, V., Radchenko, V., Engler, R., Klein, C., "Application of the PSP for Investigation of the Oscillating Pressure Fields" AIAA Paper 98-2503, 20th Advanced Measurement & Ground Testing Meeting, Albuquerque, NM, June 15-18, 1998.
10. Bell, J.H., Schairer, E.T., Hand, L.A., Mehta, R.D., "Surface Pressure Measurements Using Luminescent Coatings" Annual Reviews of Fluid Mechanics, Vol. 33, pp. 155-206, 2001.
11. Trosin, J., Hermstad D., Bell J., PAINTCP V2.2 User's Guide, Sterling (Software) Technical Note TN-93- 8006-000-48, Sept. 1, 1994.
12. Barlow, J. B., Rae, W. H., and Pope, A., Low Speed Wind Tunnel Testing, pp. 367-427, 3rd edition, John Wiley & Sons, New York, 1999.
13. Rayle, R. E., "Influence of Orifice Geometry on Static Pressure Measurements" ASME Paper 59-A-234, dec. 1959; See also M.I.T. Master's Thesis, 1949.
14. Watanabe, M., Haratia, M., Hayashi, E., "The Effect of Body Shapes on Wind Noise" SAE Paper 780266, SAE Congress, Detroit, MI, March, 1978.
15. Haruna, S., Nouzawa, T., Kamimoto, I., Sato, H., "An Experimental Analysis and Estimation of Aerodynamic Noise Using a Production Vehicle" SAE Paper 900316, SAE Congress, Detroit, MI, March, 1990.
16. Haruna, S., Hashiguchi, M., Kamimoto, I., Kuwahara, K., "Numerical Study of Aerodynamic Noise Radiated from a Three-Dimensional Wing" SAE Paper 920341, SAE Congress, Detroit, MI, March, 1992.
17. Bannister, M., "Drag and Dirt Deposition Mechanisms of External Rear View Mirrors and Techniques used for Optimization" SAE Paper 2000-01-0486, SAE Congress, Detroit, MI, March, 2000.