Three-dimensional three-temperature simulations of colliding supersonic plasma flows from irradiated CH mesh targets produce a persistent shocked turbulent mixing layer that evolves toward an isothermal state with anisotropic Reynolds stress and effective Reynolds number around 200.
A Brief Introduction to Bulk Viscosity of Fluids,
2 Pith papers cite this work, alongside 3 external citations. Polarity classification is still indexing.
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Varying weight factors in Park's two-temperature model significantly affects property distributions and heat flux for FIRE II Earth reentry cases but has little impact on Mars Pathfinder flows, with some effect visible in all cases.
citing papers explorer
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Numerical simulations of shock-driven, supersonic turbulence in colliding three-temperature laboratory plasmas
Three-dimensional three-temperature simulations of colliding supersonic plasma flows from irradiated CH mesh targets produce a persistent shocked turbulent mixing layer that evolves toward an isothermal state with anisotropic Reynolds stress and effective Reynolds number around 200.
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Influence of Park's Two-Temperature Model Control Temperature on the Flow Properties in Hypersonic Reentry Conditions
Varying weight factors in Park's two-temperature model significantly affects property distributions and heat flux for FIRE II Earth reentry cases but has little impact on Mars Pathfinder flows, with some effect visible in all cases.