NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Computational procedure for finite difference solution of one-dimensional heat conduction problems reduces computer timeComputational 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.
Document ID
19660000564
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Iida, H. T.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Electronic Components And Circuits
Report/Patent Number
MSC-1120
Accession Number
66B10566
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available