NASA NTRS ยท 19890044645
Mesh-matrix analysis method for electromagnetic launchers
Abstract
The mesh-matrix method is a procedure for calculating the current distribution in the conductors of electromagnetic launchers with coil or flat-plate geometry. Once the current distribution is known the launcher performance can be calculated. The method divides the conductors into parallel current paths, or meshes, and finds the current in each mesh by matrix inversion. The author presents procedures for writing equations for the current and voltage relations for a few meshes to serve as a pattern for writing the computer code. An available subroutine package provides routines for field and flux coefficients and equation solution.
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Elliott, David G.. 1989-01-01. Mesh-matrix analysis method for electromagnetic launchers. https://ntrs.nasa.gov/citations/19890044645
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