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.
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference9 articles.
1. Goulard, R. 1963 Radiation Transfer Regimes in Hypersonic Flight. AGARD Combustion and Propulsion Panel meeting .
2. Goulard, R. 1961 J. Quantitative Spectroscopy and Radiative Transfer,1,249.
3. Goulard, R. 1962 High temperature aspects of hypersonic flow. AGARD Fluid Dynamics Panel meeting .
4. Bird, G. A. 1960 J. Aerospace Sci. 27,713.
5. Kennet, H. 1962 ARS J. 32,1616.
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