Analysis of radiometric, lifetime and fluorescent lifetime imaging for pressure sensitive paint

Aeronautical Journal

Volumn 102, Issue 1014, 1998, Pages 189-194

  Holmes, J W ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ERROR ANALYSIS; FLUORESCENCE; PRESSURE EFFECTS; RADIOMETRY;

PRESSURE SENSITIVE PAINTS;

LUMINOUS PAINT;

EID: 0032045394     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (13)

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2. KAVANDI, J. Luminescent barometry in windtunnels. Rev Sci Inst, Nov 1990, 61, (11).
3. ENGLER, R.H. et al Description and assessment of a new optical pressure measurement system (OPMS) demonstrated in the high speed windtunnel of DLR in Gottingen, DLR Paper FB-92-24, ISBN 0939-2963, 1992.
4. SELLERS, M.E. and BRILL, J.A. Demonstration test of pressure sensitive paint in the AEDC 16 ft transonic windtunnel using the TST model, AIAA Paper 94-2481, June 1994.
5. STERN, V.O. and VOLMER, M. Uber aie abklingungszeit der fluoreszenz, Physik Zeicher XX, 1919.
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9. LAKOWICZ, J.R. et al Fluorescent lifetime imaging, Analytical Biochemistry, 1992, 202, pp 316-330.
10. MORGAN, C.G. Measurement of luminescence, US Patent 5, 459, 323, October 1995.
11. OGLESBY, D.M., PURAM, C.K. and UPCHURCH, B.T. Optimisation of measurements with pressure sensitive paints, NASA TM 4695, June 1995.
12. HOLMES, J.W. The relevance of pressure sensitive paint to aerodynamic research, J Fluorescence, 1993, 3, (3).
13. MORRIS M.J. et al Aerodynamic applications of pressure sensitive paint, AIAA Paper 92-0264. January 1992.