Characterization of pressure sensitive paint intrusiveness effects on aerodynamic data

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Amer, Tahani R ^a   Liu, Tianshu ^a   Oglesby, Donald M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ANGLE OF ATTACK; DESIGN OF EXPERIMENTS; LUMINOUS PAINT; NASA; PAINT; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; SURFACE ROUGHNESS;

AERODYNAMIC CHARACTERISTICS; LOCALIZED EFFECTS; LOW SURFACE ROUGHNESS; NASA LANGLEY RESEARCH CENTER; PRESSURE SENSITIVE PAINTS; TURBULENCE PRESSURE; WIND TUNNEL MODELING; WIND TUNNEL TESTS;

WIND TUNNELS;

EID: 85086490054     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-556     Document Type: Conference Paper

References (13)

1. B. C. Crites, (1993), Measurement Techniques - Pressure Sensitive Paint Technique, Lecture Series 1993-05, von Karman Institute for Fluid Dynamics.
2. K. S. Schanze, B. F. Carroll, S. Korotkevitch, M. J Morris., Temperature Dependence of Pressure Sensitive Paints* AIAA Journal (0001- 1452), vol. 35, no. 2
3. V. E. Mosharov, V. Radchenko, and A. Orlov, Binary Pressure Sensitive Paint: A Lot of Problems? 7th Annual PSP Workshop, Purdue University, West Lafayette, LA, Oct 11-13, 1999.
4. T. R. Amer, C. Obara, W. Goodman, B. Sealey, C. Burkett, B. Leighty, T. Carmine, Pressure Sensitive paint measurement in NASA-Langley Wind Tunnels Proceedings of the 45* International Instrumentation Symposium, May 1999, pp. 325-334.
5. E. T. Schairer, R. D. Mehta, M.E. Olsen, L. A. Hand, J. H. Bell, P. J. Whittaker, D.G. Morgan, The Effects of Thin Paint Coatings on the Aerodynamics of Semi-Span Wings, AIAA Paper 98-0587, January. 98.
6. M. E. Seller, Pressure sensitive Paint Data on the Transonic Technology Wing Demonstrator (TST) in the AEDC Propulsion Wind Tunnel 16T,AEDCTR-98-3.
7. F. G. Vanhoutte, P. R. Ashill, and K. P. Garry, Intrusion Effects of Pressure Sensitive Paint in Wind-Tunnel Tests on Wings, AIAA Paper 2000-2525, June 2000.
8. Y. Mebarki, M. Grenier, J. Than, Comparison of Pressure Sensitive Paints on A Supercritical Wing at Cruise Speed, 9th International Symposium on Flow Visualization, Paper number 207, 2000.
9. R. DeLoach," Application of Modern Experimental Design to Wind Tunnel Testing," AIAA Paper 98-0713, January 1998.
10. R. DeLoach," Improved Quality in Aerospace Testing Through the Modern Design of Experiments," AIAA Paper 2000-0825, January 2000.
11. R. DeLoach," The Modern Design of Experiments: A Technical and Marketing Framework," AIAA Paper 2000-2691, June 2000.
12. H. Schichting, " Boundary-Layer Theory," McGraw-Hill, Inc., New York, 1979.
13. DeLoach, R. "Improved Quality in Aerospace Testing Through the Modern Design of Experiments". AIAA 2000-0825. 38th AIAA Aerospace Sciences Meeting and Exhibit. Reno, NV. Jan 2000.