MSC.Dytran is a general purpose, explicit finite element analysis program
for simulating the nonlinear dynamic response of structures and mechanical components.
As an added benefit, MSC.Dytran can also be used to effectively simulate more
complex nonlinear analysis problems, such as material flow and coupled fluid-structure
interaction. The simulation of this latter class of problems is available as an
option to the basic MSC.Dytran structural analysis package.
The
technology in MSC.Dytran is based on proven numerical algorithms that
have been rigorously tested and verified in many industrial applications.
The explicit FEA technology for solving nonlinear structural analysis
problems is based primarily on algorithms originally developed at the
Lawrence Livermore Laboratory and subsequently enhanced by MSC. This technology
has traditionally been used to solve structural analysis problems involving
large displacements, nonlinear stress/strain behavior, and contact.
In contrast, the material flow and coupled fluid-structure
interaction technology in MSC.Dytran was developed entirely at MSC, and is based
on an Eulerian formulation. The foundation for this technology came from MSC's
1990 acquisition of Pisces International and the PISCES software program, originally
developed to solve complex fluid-structure interaction problems in the nuclear
and defense industries.
Key
Features
Structural
Analysis Solver MSC.Dytran employs classic explicit finite
element technology to solve dynamic structural analysis problems. The program
includes all of the necessary element types and material models to solve a wide
variety of practical engineering problems, including problems involving 3-D contact
and sliding effects. Typical applications in this category of problems are structural
crashworthiness analysis, component drop test simulation, tri-hub burst containment
analysis, and sheet metal stamping.
Element
Library
- truss element (CROD)
- beam elements
(CBEAM, CBAR)
- Belytschko-Schwer formulation
- Hughes-Liu formulation
- extensive cross section library
- seat belt element
- spot weld element
- quadrilateral shell elements (CQUAD4)
- Belytschko-Tsay formulation
- Hughes-Liu
formulation
- Key-Hoff formulation
- membrane formulation
|
- triangular shell elements (CTRIA3)
- C0 formulation
- membrane formulation
- solid elements (CHEXA, CPENTA, CTETRA)
- spring/damper
elements (CELAS, CDAMP)
- linear
- nonlinear
- corotational
- user
defined
- concentrated grid point masses (CONM2)
|
Material
Models
- isotropic linear elastic
- orthotropic linear elastic
- viscoelastic
- von Mises plasticity
- Johnson and Cook plasticity
- Krieg anisotropic
plasticity
| - soil and crushable foam
- low density foam
- rubber
- layered composites
- tabular stress/strain input
- strain rate
dependence
|
Failure
Models
- maximum effective plastic strain
- maximum effective
stress
- spalling (tension failure)
- user defined failure
|
- layered composites failure
- Tsai-Hill
theory
- Tsai-Wu theory
- Modified Tsai-Wu theory
- Maximum
Stress theory
- Chang-Chang theory
- Hashin theory
|
Equations
of State
- constant bulk modulus
- general polynomial
- ideal gas
Contact
- master-slave contact
- surface to surface
- grid points to surface
- single surface contact
- adaptive (eroding) contact
- Coulomb friction
- shell thickness offset and gaps
Rigid Bodies
- analytically defined rigid ellipsoids
- arbitrarily shaped rigid bodies
- defined via rigid surfaces
- defined via a rigid material
Constraints
- single point constraints (SPC)
- rigid grid point connections (RBE2)
- rigidly
tied surfaces
- rigid wall
- breakable connection between grid points
- kinematic
connection between shell and solid element grid points
- mechanical joints to
connect rigid bodies
Loading
- concentrated forces and moments
- follower forces and moments
- pressure
loads
- gravity loading
- centrifugal force loads
- enforced velocity
- initial
conditions
- uniform pressure airbag
- prestress condition from MSC.NASTRAN
User
Defined Subroutines
- material failure
- pressure loading
- spring/damper behavior
- velocity constraints
- customized grid point
and element output
Occupant
Modeling
- fully integrated ATB occupant model
- coupling
to MADYMO occupant model

System
Requirements
- The Operating System level is as-built. Systems
are generally presumed to run on later versions unless specifically stated otherwise.
In some instances, later versions are also cited if they warrant special mention.
| Vendor
Model | Operating
System |
| Compaq (Digital)
Alpha | Digital UNIX 4.0 |
| | |
Hewlett-Packard 9000 (7xx,
K-Class) | HP-UX 10.20, 11.00 |
| | |
| IBM RISC 6000 |
AIX 4.1.4 |
| | |
| Intel | Windows NT 4.0 (SP3) |
| | |
| SGI R4X00/R5000 | IRIX 6.2 |
| SGI R10000 | IRIX64 6.4, 6.5 |
| | |
| Sun SPARC |
Solaris 2.5.1 |