Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn 1997, Issue , 1997, Pages 105-110

  Asai, Keisuke ^a,c   Kanda, Hiroshi ^a,c   Cunningham, Corey T ^b,d   Erausquin, Rick ^b,e   Sullivan, John P ^b,e  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b PURDUE UNIVERSITY   (United States)

^c Aircraft Aerodynamics Division   (Japan)

^d Department of Chemistry ^*

^e SCHOOL OF AERONAUTICS AND ASTRONAUTICS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CALIBRATION; CRYOGENIC EQUIPMENT; LUMINOUS PAINT; MODELS; OXYGEN; PRESSURE; SURFACES; TEMPERATURE; WIND TUNNELS;

CRYOGENIC WIND TUNNEL; IN SITU CALIBRATION; LUMINESCENT COATINGS; MACH NUMBER; PRESSURE DISTRIBUTION; PRESSURE SENSITIVE PAINT; SURFACE PRESSURE; TEMPERATURE DEPENDENCE; TEMPERATURE SENSITIVE PAINT;

PRESSURE MEASUREMENT;

EID: 0031375647     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (7)

1. McLachlan, B. G. and Bell, J. H., "Pressure-Sensitive Paint in Aerodynamic Testing", Experimental Thermal and Fluid Science , Vol. 10, 1995, pp. 470-485.
2. Liu, T., Campbell, B. T., Burns, S. P., and Sullivan, J. P., "Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics", Applied Mechanics Reviews, vol. 50, no.4, pp.227-246, April 1997
3. Campbell, B. T., Liu, T., and Sullivan, J. P., "Temperature Measurement Using Fluorescent Molecules", 6th International Symposium on Application of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, July 20-23, 1992.
4. Campbell, B. T., Liu, T., and Sullivan, J. P., "Temperature Sensitive Fluorescent Paint Systems", AIAA Paper 94-2483, June 1994.
5. Asai, K., Kanda, H., Kunimasu, T., Liu, T. and Sullivan, J. P., "Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescence Paint", J. of Aircraft, Vol. 34. No.1, Jan.-Feb. 1997, see also AIAA Paper 96-2185.
6. Asai, K., "Luminescent Coating with an Extremely High Oxygen Sensitivity at Low Temperatures", Patent Pending, July 1997, Japan.
7. Sawada, H. and Aoki, T., "NAL 10cm Cryogenic Wind Tunnel", Proc. of PICAST '1 Vol. III, Taiwan, Dec. 1993, pp.1143-1150.