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CELFE: Coupled Eulerian-Lagrangian Finite Element program for high velocity impact. Part 1: Theory and formulationA 3-D finite element program capable of simulating the dynamic behavior in the vicinity of the impact point, together with predicting the dynamic response in the remaining part of the structural component subjected to high velocity impact is discussed. The finite algorithm is formulated in a general moving coordinate system. In the vicinity of the impact point contained by a moving failure front, the relative velocity of the coordinate system will approach the material particle velocity. The dynamic behavior inside the region is described by Eulerian formulation based on a hydroelasto-viscoplastic model. The failure front which can be regarded as the boundary of the impact zone is described by a transition layer. The layer changes the representation from the Eulerian mode to the Lagrangian mode outside the failure front by varying the relative velocity of the coordinate system to zero. The dynamic response in the remaining part of the structure described by the Lagrangian formulation is treated using advanced structural analysis. An interfacing algorithm for coupling CELFE with NASTRAN is constructed to provide computational capabilities for large structures.
Document ID
19790021661
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, C. H.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-159395
LMSC-HREC-TR-D497204-PT-1
Report Number: NASA-CR-159395
Report Number: LMSC-HREC-TR-D497204-PT-1
Accession Number
79N29832
Funding Number(s)
CONTRACT_GRANT: NAS3-18908
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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