Blowdown tunnel application of pressure sensitive paint

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 531-540

  Shimbo, Yuichi ^a   Noguchi, Masayoshi ^a   Makino, Yoshikazu ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ATMOSPHERIC TEMPERATURE; CCD CAMERAS; LUMINOUS PAINT; OCEANOGRAPHY; SUPERSONIC AERODYNAMICS; WIND TUNNELS;

PAINT TECHNIQUES; PRESSURE FIELD; PRESSURE SENSITIVE PAINTS; SUPERSONIC WIND TUNNEL; SURFACE TEMPERATURES; TEMPERATURE AND PRESSURES; TEMPERATURE SENSITIVE PAINT; TEMPERATURE SENSITIVITY;

PAINT;

EID: 84964238293     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Asai K., Kanda H., and Iijima Y., "Luminescence Characteristics of Pressure Sensitive Paint Based on Platinum Octaethylporphyrin", Proc. of the 23rd Symposium on Visualization, J. of Flow Vis. Soc. of Japan, Vol. 15, Suppl. No. 1, 1995 (in Japanese).
2. Asai K, Kanda H., Iijima Y, Lee S. and Okura I., "Sample Tests of Pressure-Sensitive Paints with 49 Different Formulations", Proc. of the 25th Symposium on Visualization, J. of Flow Vis. Soc. of Japan, Vol. 17, Suppl. No. 1, 1997 (in Japanese).
3. Asai K, Kanda H., Cunningham C., Erausquin R. and Sullivan J., "Surface Pressure Measurement in a Cryogenic Wind Tunnel by Using Luminescent Coating", 17th ICIASF, Sept., 1997
4. Liu T., Johnston R., Torgerson S., Fleeter S. and Sullivan J., "Rotor Blade Pressure Measurement in a High Speed Axial Compressor Using Pressure and Temperature Sensitive Paint", AIAA-97-0162
5. Shimbo Y, Asai K., Kanda H., Iijima Y, Komatsu N., Kita S. and Ishiguro M., Evaluation of Several Calibration Techniques of Pressure Sensitive Paint at Transonic Testing, AIAA-98-2502
6. Shimbo Y., Noguchi M., Iijima Y. and Asai K, Blowdown Tunnel Application of Pressure Sensitive Paint (Preliminary Test), 6th Pressure Sensitive Paint Workshop, Renton, Oct., 1998
7. Yoshida K., Overview of NAL’s Program Including the Aerodynamic Design of the Scaled Supersonic Experimental Airplane, RTO-EN-4, Nov. 1998
8. McLachlan B. G, Kavandi J. L., Callis J. B., Gouterman M., Green E., Khalil G. and Burns D., "Surface pressure field mapping using luminescent coatings", Experiments in Fluids 14 (1993)
9. Liu T., Campbell B. T, Burns S. P. and Sullivan J. P., "Temperature and Pressure-Sensitive Luminescent paints in Aerodynamics", Apl. Mech. Rev., Vol. 50, No. 4, 1997
10. Baron A. E., Danielson J. D. S., Gouterman M., Wan J. R, Callis J. B. and McLachlan B., "Submillisecond response times of oxygen-quenched luminescent coatings", Rev. Sci. Instrum. 64 (12), Dec. 1993, pp. 3394-3402
11. Crites R. C., "Measurement Techniques - PRESSURE SENSITIVE PAINT TECHNIQUE", von Karman Institute for Fluid Dynamics, Lecture series 1993-05
12. Ponomarev S., and Gouterman M., Fast Responding Pressure Sensitive Paints Based on High Concentration of Hard Particles in Polymer, 6th Pressure Sensitive Paint Workshop, Renton, Oct., 1998