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RETSCP: A computer program for analysis of rocket engine thermal strains with cyclic plasticityA computer program, designated RETSCP, for the analysis of Rocket Engine Thermal Strain with Cyclic Plasticity is described. RETSCP is a finite element program which employs a three dimensional isoparametric element. The program treats elasto-plastic strain cycling including the effects of thermal and pressure loads and temperature dependent material properties. Theoretical aspects of the finite element method are discussed and the program logic is described. A RETSCP User's Manual is presented including sample case results.
Document ID
19740026131
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miller, R. W.
(Atkins and Merrill, Inc. Ashland, MA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-134640
Report Number: NASA-CR-134640
Accession Number
74N34244
Funding Number(s)
CONTRACT_GRANT: NAS3-17807
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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