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Measurements of heat transfer in separated highenthalpy dissociated laminar hypersonic flow behind a step

Published online by Cambridge University Press:  26 April 2006

S. L. Gai
Affiliation:
University College, UNSW, Australian Defence Force Academy, Canberra, Australia
N. T. Reynolds
Affiliation:
University College, UNSW, Australian Defence Force Academy, Canberra, Australia
C. Ross
Affiliation:
University College, UNSW, Australian Defence Force Academy, Canberra, Australia
J. P. Baird
Affiliation:
University College, UNSW, Australian Defence Force Academy, Canberra, Australia

Abstract

Measurements of heat transfer in the separated region behind a rearward-facing step in a hypersonic high-enthalpy stream, are described. The range of enthalpies considered was much greater than those reported previously in the literature. High-response surface thermocouples were used to measure the heat-transfer rates. Flow visualization by way of interferograms, with a Mach-Zehnder interferometer, were obtained and improved visualization was further facilitated by digitizing the interferograms and using Fourier analysis to determine fringe positions. This then provided a phase map of the flow region in which the phase was colour coded to emphasize flow characteristics.

Type
Research Article
Copyright
© 1989 Cambridge University Press

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References

Back, L. H. & Cuffel, R. F., 1970 AIAA J. 8, 19711873.
Baird, J. P., Lyons, P. R. A. & Gai, S. L. 1985 AIAA 20th Thermophysics Conf., Willamsburt Virginia, USA
Baird, J. P., Gai, S. L. & Reynolds, N. T., 1986. Proc. 4th Intl Symp. on Flow Visualisation, Paris pp. 549553. Hemisphere.
Baker, P. J. & Martin, B. W., 1986 Intl J. Heat Mass Transfer 9, 10811088.
Chapman, D. R.: 1956 NACA Tech. Note 3792.
Charwat, A. F., Dewey, C. F., Roos, J. N. & Hitz, J. A., 1961a J. Aerospace Sci. 6, 457470.
Charwat, A. F., Dewey, C. F., Roos, J. N. & Hitz, J. A., 1961b J. Aerospace Sci. 7, 513527.
Coleman, G. T. & Stollery, J. L., 1972 J. Fluid Mech. 56, 741752.
Crane, K. C. A. & Stalker, R. J. 1977 J. Phys. D Appl. Phys. 10, 679695.
East, R. A., Stalker, R. J. & Baird, J. P., 1980 J. Fluid Mech. 97, 673699.
Hama, F. R.: 1968. AIAA J. 6, 212219.
Lordi, J. A., Mates, R. E. & Moselle, J. R., 1966 NASA CR-472.
Lyons, P. R. A. & Gai, S. L. 1988 J. Phys. E Sci. Instrum. 21, 445448.
Naysmith, A.: 1961 Proc. Intl Heat Transfer Conf. London, vol. 43, p. 378. ASME-Inst. Mech. Engrs.
Nestler, D. E.: 1985 AIAA 20th Thermophysics Conf., Williamsburg, Virginia, USA.
Reynolds, N. T.: 1985 Flow over a rearward facing step in high enthalpy hypersonic flow. Final year B. E. thesis.
Richards, B. E. & Stollery, J. L., 1979 J. Aircraft 16, 177181.
Roberts, G. T.: 1984 University of Southampton, Rep. AASU Mem. 84/7.
Rogers, E. W. E., Metcalf, S. C. & Berry, C. J., 1967 Aero. Res. Counc. R&M 3506.
Rom, J. & Seginer, A., 1964 AIAA J. 2, 251255.
Ross, C.: 1986. High Mach number airflow behind a rearward facing step. Final year B. E. thesis.
Sandford, J. & Ginoux, J. J., 1968. Von Karman Institute Tech. Note 38.
Schultz, D. L. & Jones, T. V., 1973 AGARD Rep. 165.
Shang, J. S. & Korkegi, R. H., 1968 AIAA J. 6, 986987.
Stalker, R. J.: 1985 Free piston Shock Tunnel T3, Facility Hand Book, Univ. of Qld.
Wada, I. & Inoue, Y., 1973 10th Intl Symp. on Space Tech. and Science, Tokyo.
Weiss, R. F. & Weinbaum, S., 1966 AIAA J. 4, 13211330.
White, F. M.: 1974 Viscous Fluid Flow, p. 589. McGraw-Hill.
Wyborny, W., Kabelitz, H. P. & Schepers, H. J., 1967 AGARD Conf. Proc. 19.