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...one of the most advanced simulation tools for nonlinear structural analysis!

Analysis Capabilities
LS-DYNA is a multi-purpose, explicit and implicit finite element program used to analyze linear and nonlinear static and dynamic behavior of physical procedures. The main capabilities of LS-DYNA are
Nonlinear Dynamics |
Parallel Processing (SMP, MPP) |
Explicit and Implicit Time-Stepping |
Eigenvalue Analysis |
Adaptive Mesh Refinement |
Thermal Analysis |
Fluid Dynamics |
Arbitrary Lagrangian-Eulerian (ALE) |
Fluid-Structure Interaction |
Failure Analysis |
Crack Propagation |
Fully Automated Contact Analysis |
Quasi-Static Simulations |
FEM to Rigid Multi-Body Dynamics Coupling |
Real-Time Acoustics |
Multi-Physics Coupling (structural, thermal fluid, acoustics, etc.) |
Smooth Particle Hydrodynamics (SPH) |
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Contact
The fully automated contact analysis capability in LS-DYNA is easy to use, robust, and validated. It uses constraint and penalty methods to satisfy contact conditions. These techniques have worked extremely well over the past twenty years in numerous applications such as full-car crashworthiness studies, system/component analysis, and occupant safety analysis. Coupled thermo-mechanical contact can also be handled.
Over fourty different contact options are available. These options primarily treat contact of: deformable to deformable bodies, single surface contact in deformable bodies, and deformable body to rigid body contact. Multiple definitions of contact surfaces are possible, for example:
Singel Surface Contact
Contact with Rigid Walls
Tied Surfaces
Nodes Tied to Surfaces
Shell Edges Tied to Shell Surfaces
Fluid-Structure Interfaces
Eroding Contact
Edge-to-Edge Contact
Resultant Force Contact
Draw Beads
Contact with CAD Surfaces
A special option exists for treating contact between a rigid surface (usually defined as an analytical surface) and a deformable structure. On example is in metal forming, where the punch and die surface geometries can be input as IGES- or VDA-surfaces which are assumed rigid. Another example is in occupant modeling, where the rigid-body occupant dummy (made up of geometric surfaces) contacts deformable structures such as airbags and instrument panels.
Several friction models are available:
Static and Dynamic Coulomb Friction
Viscous Friction
Pressure Dependent Friction
User-Defined Friction Models
Contact input is made easier by allowing contact to be defined by part identifiers, by box, or by simply including the entire model in the contact definition.
Material Models
LS-DYNA has over 130 metallic and non-metallic material models.
Elastic |
Elasto-Viscoplastic |
Elastomers |
Foam Models |
Linear Visco-Elasticity |
Glass Models |
Geological Models |
Fabric Material/Element |
Kevlar Material with Damage |
Equations-of-State Hydrodynamic Models |
Acoustic Pressure Material/Element |
Biomechanic Material Models |
Composites |
Special Capabilities for Fluid Analysis |
User-Defined Materials |
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Element Library
The lower-order finite elements in LS-DYNA are accurate, simple and efficient. For the under-integrated shell and solid elements, zero-energy modes are controlled by either an hourglass viscosity or stiffness. All elements are nearly 100% vectorized.
Beams
Hughes-Liu Beam
Belytschko-Schwer Resultant Beam
Truss Element
Belytschko-Schwer Beam with full cross-section integration
Belytschko-Schwer Tubular Beam
Discrete Beam / Cable
2D Plane Strain Shell Element
2D Axisymmetric Volume Weighted Shell Element
Spotweld Beam
Discrete Elements
Spring (translational and torsional)
Damper (translational and torsional)
Seatbelt Elements
Accelerometer
Pretensioner
Retractor
Sensor
Slipring
4-Node Thin Shells
Hughes-Liu Shell
Belytschko-Tsay Shell
Belytschko-Leviathan Shell
Belytschko-Wong-Chiang Shell
Fully Integrated Shells
Plane Stress Shell
Triangular Shells
C0 Shell
DKT Shell
Membranes
Belytschko-Tsay Membrane
Fully Integrated Belytschko-Tsay Membrane
Solids
8-Node Brick Element
4-Node Tetrahedron Element
Arbitrary Lagrangian-Eulerian (ALE) Brick Element
Eulerian Brick Element
Eulerian Navier-Stokes Element
8-Node Thick Shells
Reduced Integration
Selective Reduced Integration
Solids
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