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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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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Abstract 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.
AbstractList 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.
Author Gilligan, J.G.
Orton, N.P.
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  fullname: Gilligan, J.G.
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Snippet 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...
SourceID ieee
SourceType Publisher
StartPage 235
SubjectTerms Computer interfaces
Electrothermal launching
Equations
Magnetic liquids
Plasma temperature
Plasma transport processes
Power engineering and energy
Railguns
Railway engineering
Steady-state
Title A boundary layer model of energy transport at plasma-surface interfaces in railguns
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