Article contents
Effect of radiative heat loss on steady hypersonic flow past a blunt body
Published online by Cambridge University Press: 28 March 2006
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
- Information
- Copyright
- © 1967 Cambridge University Press
References
- 3
- Cited by