Dyna3d

This information is from here: http://www.oecd-nea.org/tools/abstract/detail/nesc9909/

(I ran my PhD models using this software on a Cray X-MP at the University of London Computer Centre )

NESC9909 DYNA3D.

DYNA3D, 3-D Finite Elements for Dynamic Response of Inelastic Solids

3. DESCRIPTION OF PROGRAM OR FUNCTION

DYNA3D is an explicit, three- dimensional, finite element program for  analyzing the large deformation dynamic response of inelastic solids and structures. DYNA3D contain 30 material models and 10 equations of state (EOS) to cover a wide range of material behavior. The material models  implemented are: elastic, orthotropic elastic, kinematic/isotropic  plasticity, thermoelastoplastic, soil and crushable foam, linear viscoelastic, Blatz-Ko rubber, high explosive burn, hydrodynamic without deviatoric stresses, elastoplastic hydrodynamic, temperature dependent elastoplastic, isotropic elastoplastic, isotropic elastoplastic with failure, soil and crushable foam with failure, Johnson/Cook plasticity model, pseudo TENSOR geological model, elastoplastic with fracture, power law isotropic plasticity, strain¬ ¬ rate dependent plasticity, rigid, thermal orthotropic, composite damage model, thermal orthotropic with 12 curves, piecewise linear isotropic plasticity, and inviscid two invariant geologic cap, orthotropic crushable model, Moonsy-Rivlin rubber, resultant plasticity, closed form update shell plasticity, and  Frazer-Nash rubber model. The IBM 3090 version does not contain the last two models mentioned.

The hydrodynamic material models determine only the deviatoric stresses. Pressure is determined by one of ten equations of state including linear polynomial, JWL high explosive, Sack "Tuesday" high explosive,  Gruneisen, ratio of polynomials, linear polynomial with energy  deposition, ignition and growth of reaction in HE,  tabulated¬ ¬ compaction, tabulated, and TENSOR pore collapse. DYNA3D generates three binary output databases. One contains information for  complete states at infrequent intervals; 50 to 100 states is typical.  The second contains information for a subset of nodes and elements at frequent intervals; 1,000 to 10,000 states is typical. The last contains interfaces data for contact surfaces.

This package is distributed by:
Energy Science and Technology Software Center
P.O. Box 62
1 Science.Gov Way
Oak Ridge, TN 37831
(865) 576-2606 TEL
(865) 576-6436 FAX
E-mail: ESTSC@osti.gov

4. METHOD OF SOLUTION

A contact-impact algorithm permits gaps and sliding along material interfaces with friction. All versions except for the IBM3090 include an interface type defining one-way treatment of sliding with voids and friction. By a specialization of this algorithm, such interfaces can be  rigidly tied to admit variable zoning with no need for transition regions. Spatial discretization is achieved by implementation of  Hughes-Liu rectangular beams and shells, Belytschko-Tsay shells and beams, triangular shell elements¬ ¬ based on work by Belytschko and  colleagues, and 8-node solid-shell elements. All element classes can be included as parts of a rigid body. Three-dimensional plane stress  constitutive subroutines update the stress tensor for the shell elements such that the stress component normal to the shell midsurface is zero.  One constitutive evaluation is made for each integration point through the shell thickness. The 8-node solid element uses either one point integration or the Flanagan and Belytschko constant stress formulation with exact volume integration. Zero energy modes in the¬ ¬ shell and solid elements are controlled by either an hourglass viscosity of stiffness. The equations of motion are integrated in time by the central difference method. A Jaumann stress rate formulation is used with the exception of the orthotropic elastic and the rubber material subroutines which use  Green-St.Venant strains to compute second Piola-Kirchoff stresses which transform to Gauchy stresses.

5. RESTRICTIONS ON THE COMPLEXITY OF THE PROBLEM

Storage allocation is dynamic. The only limit that exists is the storage capacity of the computer. Typical calculations have 10,000 to 200,000 elements.

6. TYPICAL RUNNING TIME

Execution speeds on the Cray X-MP for various DYNA3D element types range from 4 to 48 microseconds per element cycle. These timings are approximate and do not account for the inclusion of sliding interfaces or complex material models. Typical¬ ¬ problems require from 4 to 80 minutes on the Cray X-MP.

7. UNUSUAL FEATURES OF THE PROGRAM:

8. RELATED AND AUXILIARY PROGRAMS

The soil and crushable foam, linear viscoelastic, and the rubber Blatz-Ko subroutines were adapted from¬ ¬ HONDO and recoded for  vectorization, the ignition and growth EOS was adapted from KOVEC. The  forms of the first five equations of state are from KOVEC also. The three-dimensional contact-impact algorithm¬ ¬ is an extension of the NIKE2D (NESC9923) two-dimensional algorithm.¬ ¬ The tied and sliding only  interface options are similar to the two-¬ ¬ dimensional algorithm used in DYNA2D (NESC9910). DYNA3D relies on stand-alone mesh generators. INGRID (NESC9649) is recommended for creation of input files, since it  provides complete support for all slide surface data, boundary  conditions, loads, material properties, and control parameters. The  compatible release of TAURUS (NESC9908) processes DYNA3D output plotting contours, fringes, time histories, and deformed shapes. A variety of strain measures, reaction forces along constrained boundaries, and  momenta¬ ¬ can be computed.

9. STATUS

No status

10. REFERENCES

- D.W. Stillman and J.O. Hallquist
INGRID: A Three-Dimensional Mesh Generator for Modeling Nonlinear
Systems,
UCID-20506, July 1985.
- J.P. Woodruff
KOVEC User's Manual,
UCID-17306, November 23, 1976.
- Michael A. Gerhard
SLIC: An Interative, Graphic Mesh Generator for Finite-Element and Finite Difference Applications Programs,
UCRL-52823, September 13, 1979.
- DYNA3D, NESC No. 9909.CRA1B, DYNA3D Edition B Cray Tape
Description
National Energy Software Center Note 90-50, March 30, 1990.
- DYNA3D, NESC No. 9909.VAX, DYNA3D DEC VAX Version Tape Description National Energy Software Center Note 90-51, March 30,  1990.

11. MACHINE REQUIREMENTS:

12. PROGRAMMING LANGUAGE(S) USED

No specified programming language

13. OPERATING SYSTEM UNDER WHICH PROGRAM IS EXECUTED

COS (Cray), VMS (DEC VAX11), VM/MVS (IBM3090), UNIX BSD 4.2 (SUN).

14. OTHER PROGRAMMING OR OPERATING INFORMATION OR RESTRICTIONS

Presently, only parts of the sliding interface logic are vectorized.

15. NAME AND ESTABLISHMENT OF AUTHORS

R.G. Whirley
Lawrence Livermore National Laboratory
P.O. Box 808
Livermore, California 94550


T. Kennedy
IBM Corporation

16. MATERIAL AVAILABLE

 

17. CATEGORIES

  • I. Deformation and Stress Distributions, Structural Analysis and Engineering Design Studies

Keywords: deformation, dynamic loads, finite element method, hydrodynamics, solids, three-dimensional.

 

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