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Effect of radiative heat loss on steady hypersonic flow past a blunt body

Published online by Cambridge University Press:  28 March 2006

M. I. G. Bloor
Affiliation:
Department of Mathematics, University of Leeds

Abstract

Using the grey gas approximation, the effect of radiative heat loss on axially symmetric flows is studied. Using an expansion procedure about the axis of symmetry, a numerical solution for the stagnation region is found taking the shock to be spherical. The results of this calculation are compared with the results of Lighthill's non-radiative constant density solution.

Type
Research Article
Copyright
© 1967 Cambridge University Press

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References

Bird, G. A. 1960 J. Aerospace Sci. 27, 713.
Chandrasekar, S. 1960 Radiative Transfer. New York: Dover.
Goulard, R. 1961 J. Quantitative Spectroscopy and Radiative Transfer, 1, 249.
Goulard, R. 1962 High temperature aspects of hypersonic flow. AGARD Fluid Dynamics Panel meeting.
Goulard, R. 1963 Radiation Transfer Regimes in Hypersonic Flight. AGARD Combustion and Propulsion Panel meeting.
Goulard, R. 1964 Supersonic Flow, Chemical Processes and Radiative Transfer.
Kennet, H. 1962 ARS J. 32, 1616.
Lighthill, M. J. 1957 J. Fluid Mech. 2, 1.
Thomas, P. D. 1962 Aerospace Sci. 29, 477.