Temperature measurements in a hypersonic boundary layer using planar laser-induced fluorescence

AIAA journal

Volumn 38, Issue 9, 2000, Pages 1769-1772

  Palma, P C ^a   Mallinson, S G ^a,c   O'Byrne, S B ^a   Danehy, P M ^a   Hillier, R ^b  

^a AUSTRALIAN NATIONAL UNIVERSITY   (Australia)

^b IMPERIAL COLLEGE LONDON   (United Kingdom)

^c UNIVERSITY OF TECHNOLOGY SYDNEY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLUORESCENCE; HYPERSONIC FLOW; LAMINAR FLOW; NAVIER STOKES EQUATIONS; TEMPERATURE MEASUREMENT;

PULSED LASER INDUCED FLUORESCENCE;

BOUNDARY LAYER FLOW;

EID: 0034275914     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1172     Document Type: Article

References (10)

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2. Baird, J. P., Lyons, P. R. A., and Gai, S. L., "Density and Velocity Profiles in Nonequilibrium Laminar Boundary Layers in Air," AIAA Paper 85-0976, 1985.
3. Mallinson, S. G., Gai, S. L., and Mudford, N. R., "The Boundary Layer on a Flat Plate in Hypervelocity Flow," Aeronautical Journal, Vol. 100, No. 2, 1996, pp. 135-141.
4. Eckbreth, A. C., Laser Diagnostics for Combustion Temperature and Species, 2nd ed., Gordon and Breach, 1996.
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7. Mallinson, S. G., Hillier, R., Zanchetta, M., Soltani, S., and Kirk, D., "An Experimental and Numerical Study of Hypersonic Turbulent Boundary Layers," AIAA Paper 97-2290, June 1997.
8. McIntosh, M., "Computer Program for the Numerical Calculation of Frozen Equilibrium Conditions in Shock Tunnels," Rept., Dept. of Physics, Faculties, Australian National Univ., Canberra, Australian Capital Territory, Australia, 1968.
9. Vardavas, I., "Modelling Reactive Gas Flows Within Shock Tunnels," Australian Journal of Physics, Vol. 37, 1984, pp. 157-177.
10. Palma, P. C., Danehy, P. M., and Houwing, A. F. P., "Non-Intrusive Thermometry in Shock Layers Using Multi-Line Fluorescence Imaging," 21st International Symposium on Shock Waves, Panther Publishing, Canberra, Australian Capital Territory, Australia, 1997, pp. 447-452.