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Nasa PHT

TRANSIENT RESPONSE

Transient Response of Ablating Axisymmetric Bodies Including the Effects of Shape Change


A computer program has been developed to analyze the transient response of an ablating axisymmetric body, including the effect of shape change. The governing differential equation, the boundary conditions for the analysis on which the computer program is based, and the method of solution of the resulting finite-difference equations are discussed in the documentation.


Program Size: 1,679 Statements
Computer Language: FORTRAN IV

Copyright (c) 1996 Pacific HiTech, Inc. and COSMIC