MHD Plasma Nozzle Demo

State

Solver

Method

Verbosity

Auto-update

Superconductor (SC)

Current (A)

Parabolic Cage

Count

R Throat

R Exit

Z Start

Z End

Plasma

Count

Z (t0=t1)

R Start (t0)

R End (t1)

Trajectory

Mode

t = 0.00

Visualization

Vector Field

GLSL Shader

Control Points

Rings / Profile

Field Scale

B Saturation

Energy

Usage & links
This demo solves a simplified magnetohydrodynamic (MHD) nozzle problem: coil currents shape the magnetic field and plasma radius along the axis, using flux conservation and geometric control points.
Code basis: utilities and concepts from the SimpleSimulationEngine project and its space-warfare / plasma notes (space_warfare).

MHD Nozzle