Enhanced Plasma Electrical Conductivity Modeling for Hypersonic Magnetohydrodynamic Control Simulations
Electrical Conductivity Model, Flight Altitude, Hypersonic, Plasma, Magnetohydrodynamic (MHD) Control
localized steady uniform blowing, hypersonic flow, Görtler vortices, transition delay
Chemical nonequilibrium, Computational fluid dynamics, Source term limiter, Implicit time-marching scheme, Adaptive update method
SPH-FEM coupling, shell elements, single-layer boundary condition, penalty displacement technology, multi-resolution