Pressure sensitive paint measurement in a hypersonic shock tunnel

21st Aerodynamic Measurement Technology and Ground Testing Conference

Volumn , Issue , 2000, Pages

  Nakakita, Kazuyuki ^a   Yamazaki, Takashi ^a   Asai, Keisuke ^a   Teduka, Norikazu ^b   Fuji, Atsuhiko ^b   Kameda, Masaharu ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOKYO UNIVERSITY OF AGRICULTURE AND TECHNOLOGY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; ANGLE OF ATTACK; HYPERSONIC FLOW; LUMINOUS PAINT; PRESSURE DISTRIBUTION; PRESSURE SENSORS; PRESSURE TRANSDUCERS; SUPERSONIC AERODYNAMICS; WIND TUNNELS;

ANODIZED ALUMINUM PRESSURE SENSITIVE PAINTS; DISTRIBUTION MEASUREMENT; EXPERIMENTAL MODELING; HYPERSONIC WIND TUNNELS; PRESSURE SENSITIVE PAINTS; QUANTITATIVE PRESSURES; STANDARD DEVIATION; SURFACE PRESSURE DISTRIBUTION;

PAINT;

EID: 85088756821     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-2523     Document Type: Conference Paper

References (14)

1. Edney, B., "Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock," Aeronautical research Institute of Sweden, Report 115, Feb. 1968.
2. Dolling, D. S. and Bogdonoff, S. M., "Blunt Fin-Induced Shock Wave/Turbulent Boundary-Layer Interaction," AIAA Journal, Vol. 20, No. 12, 1982, pp. 1674-1680.
3. Liu, T., Campbell, B. T., Bums, S. P., and Sullivan, J. P., 'Temperature-and Pressure-Sensitive Luminescence Paints in Aerodynamics," Applied Mechanics Reviews, Vol. 50, No. 4, April 1997, pp.227-246.
4. Sinbo, Y., Asai, K., and Komatsu, N., "Pressure Sensitive Paint Application at Large Production Wind Tunnels," 22nd ICAS Congress, Aug. 2000. (to be presented)
5. Brown, O., Mehta, R., and Cantwell, B" "-Low Speed-Pressure Sensitive Paint Research," Proceeding of the 6th Annual PSP Workshop, Oct. 1998, pp. 18.1-18.49.
6. Hubner, J., Carroll, B., Schanze, IC, and Holden, M., 'Temperature-and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow," AIAA 99-0388, Jan. 1999.
7. Borovoy, V., Bykov, A., Mosharov, V., Orlov, A., Radchenko, V., and Phonov, S., "Pressure Sensitive Paint Application in Shock Wind Tunnel," 16th ICLASF Record, 1995, pp. 34.1-34.4.
8. Asai, K., Kanda, H., Cunningham, C. T, Erausquin, R., and Sullivan, J., "Surface Pressure Measurement in a cryogenic wind tunnel by using luminescent coating," ICLASF'97 Record, Sep. 1997, pp.105-114.
9. Sakaue, H., Sullivan, J. P., Asai, K., Iijima, Y., and Kunimasu, T., "Anodized Aluminum Pressure Sensitive Paint in a Cryogenic Wind TYinnel," ISA Proceedings of the 45* International Instrum. Sym., 1999, pp. 345-354.
10. Sakaue, H. and Sullivan, J. P., "Fast Response Time Characteristics of Anodized Aluminum Pressure Sensitive Paint," AIAA-2000-0506, Jan. 2000.
11. Teduka, N., Kameda, M., Amao, Y and Asai, K., "Experimental Investigation on Time Response of Pressure-Sensitive Paint "Proceedings of the 31 th JSASS Annual Meeting, Mar. 2000, pp. 218-221. (in Japanese)
12. Soga, K., Sirouzu, M., and Yamazaki, T., "Modification of NAL Middle Scale Shock Tunnel as High Enthalpy Facility," Journal of the Japan Society for Aeronautical and Space Sciences, Vol. 42, No. 480, Jan. 1994, pp. 39-44. (in Japanese)
13. Liu, T., Guille, M., and Sullivan, J, "Uncertainty Analysis of Pressure Sensitive Paint Measurement," AIAA 99-3785, 1999.
14. Yamazaki, T., Nakakita, K., and Hozumi, K., "Aerodynamic Test of Compression Ramp in NAL Middle Scale Shock Tunnel," Proceedings of 30th Fluid Dynamics Conference, Oct. 1998, pp. 177-180. (in Japanese)