NASA NTRS · 19660000564
Computational procedure for finite difference solution of one-dimensional heat conduction problems reduces computer time
Abstract
Computational procedure reduces the numerical effort whenever the method of finite differences is used to solve ablation problems for which the surface recession is large relative to the initial slab thickness. The number of numerical operations required for a given maximum space mesh size is reduced.
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Iida, H. T.. 1966-11-01. Computational procedure for finite difference solution of one-dimensional heat conduction problems reduces computer time. https://ntrs.nasa.gov/citations/19660000564
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