Performance comparison of pressure sensitive paints

Proceedings of the International Instrumentation Symposium

Volumn 47, Issue , 2001, Pages 187-201

  Oglesby, Donald M ^a   Jordan, Jeffrey D ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Global pressure; Pressure measurement; Pressure sensitive paint

Indexed keywords

PHOTOPHYSICS; PRESSURE SENSITIVE PAINTS;

DATA REDUCTION; FINITE ELEMENT METHOD; FLUORESCENCE; PARTIAL PRESSURE; PHOSPHORS; POLYMERIZATION; PRESSURE EFFECTS; QUENCHING; VISCOSITY;

LUMINOUS PAINT;

EID: 1842538087     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. B. C. Crites,(1993), Measurement Techniques - Pressure Sensitive Paint Technique, Lecture Series 1993-05, von Karman Institute for Fluid Dynamics.
2. S. Gouin, and M. Gouterman, Ideality of Pressure Sensitive Paint II. Effect of the Diffusion Properties of Basecoats on the Luminescence Behaviour of the Sensing Layer, submitted to Macromolecules, Oct. 1998.
3. D. M Oglesby, C. K. Puram, and B. T Upchurch,. (1995a), Optimization of Measurements With Pressure Sensitive Paints, NASA TM 4695.
4. th AIAA Fluid Dynamics Conference, June 28-July 1, 1999, Norfolk, VA.
5. K. S. Schanze, B. F. Carroll, S. Korotkevitch, and M. Morris, (1997), Temperature Dependence of Pressure Sensitive Paints, AIAA J., Vol. 35, No. 2, February, 306-310.
6. K. S. Schanze, B. F Carroll, S. Korotkevitch, M. J. Morris, Concerning the Temperature Dependence of Pressure Sensitive Paints, AIAA Paper 97-0386
7. 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
8. S. Gouin, and M. Gouterman, Ideality of Pressure Sensitive Paint I. Effect of Annealing on the Temperature Dependence of the Luminescnce, submitted to Macromolecules, Oct. 1998.
9. A. Bykov, S. Fonov, V. Mosharov, A. Orlov, V. Pesetsky, and V. Radchenko, (1997), Study Result for the Application of Two-component PSP Technology to Aerodynamic Experiment, AGARD Conference Proceedings CP-601, Advanced Aerodynamic Measurement Technology, 29-1 to 29-8.
10. th AIAA Aerospace Sciences Meeting & Exhibit, January 8-11, 2001, Reno, NV.
11. nd International Instrumentation Symposium, pp 205-223, San Diego, CA, May 5-9, 1996.