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Three-dimensional finite element analysis for high velocity impactA finite element algorithm for solving unsteady, three-dimensional high velocity impact problems is presented. A computer program was developed based on the Eulerian hydroelasto-viscoplastic formulation and the utilization of the theorem of weak solutions. The equations solved consist of conservation of mass, momentum, and energy, equation of state, and appropriate constitutive equations. The solution technique is a time-dependent finite element analysis utilizing three-dimensional isoparametric elements, in conjunction with a generalized two-step time integration scheme. The developed code was demonstrated by solving one-dimensional as well as three-dimensional impact problems for both the inviscid hydrodynamic model and the hydroelasto-viscoplastic model.
Document ID
19760014504
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chan, S. T. K.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Lee, C. H.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Brashears, M. R.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-134933
LMSC-HREC-TR-D390900
Report Number: NASA-CR-134933
Report Number: LMSC-HREC-TR-D390900
Accession Number
76N21592
Funding Number(s)
CONTRACT_GRANT: NAS3-18908
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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