NASA NTRS · 19750000186
RETSCP-A computer program for analysis of rocket engine thermal strains with cyclic plasticity
Abstract
Finite element program employs three-dimensional isoparametric element for analysis of rocket engine thermal strains with cyclic plasticity.
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Miller, R. W.. 1975-10-01. RETSCP-A computer program for analysis of rocket engine thermal strains with cyclic plasticity. https://ntrs.nasa.gov/citations/19750000186
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