A boundary layer model of energy transport at plasma-surface interfaces in railguns

Summary form only given. A 2-D turbulent steady-state computer code has been developed to analyze ablation and vapor shielding processes at plasma facing surfaces in railguns and electrothermal (ET) launchers. Due to the high plasma temperature and the high Reynolds number flow, both radiation trans...

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Bibliographic Details
Published in:International Conference on Plasma Sciences (ICOPS) p. 235
Main Authors: Orton, N.P., Gilligan, J.G.
Format: Conference Proceeding
Language:English
Published: IEEE 1993
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Summary:Summary form only given. A 2-D turbulent steady-state computer code has been developed to analyze ablation and vapor shielding processes at plasma facing surfaces in railguns and electrothermal (ET) launchers. Due to the high plasma temperature and the high Reynolds number flow, both radiation transport and turbulence must be considered to accurately model energy transport to the surface. This system has been modeled using fluid boundary layer equations, including a two-equation (k-ϵ) model for turbulence and a constant magnetic field normal to the wall, coupled with thermal radiation transport. Numerical solution of the boundary layer equations follows the method of Patankar and Spalding. The code calculates the mass evolution rate at the surface and makes it possible to determine the relative importance of energy transport to the surface via radiation and turbulent convection.
ISBN:0780313607
9780780313606
ISSN:0730-9244
2576-7208
DOI:10.1109/PLASMA.1993.593653