MSC.NASTRAN Product Details

MSC.NASTRAN Product Details

Product Description
       
Optional Analysis Modules
       
       


Product Description

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MSC.NASTRAN is the industry's leading FEA program. In an area where unreliable results may cost millions of development dollars, MSC.NASTRAN has proven its accuracy and effectiveness over and over. It has remained the leading FEA program by constantly evolving to take advantage of the newest analytical capabilities and algorithms for structural analysis. MSC.FEA

MSC.NASTRAN offers a wide variety of analysis types, including linear statics, normal modes, buckling. Optional analysis modules can be added to support heat transfer, dynamics, frequency response, transient response, random response, and response spectrum analysis as your analysis requirements increase.

Virtually any material type can be modeled, including composites and hyperelastic materials. Advanced features include superelements (substructuring), component mode synthesis, and DMAP (a tool kit for creating custom solutions in support of your proprietary applications).

Superior element technology and robust numerical methods are the foundation of MSC.NASTRAN. The program includes h- and p-elements, and both can be mixed in the same model for increased modeling accuracy with minimal computer resources. The p-elements conform closely to a structure's curved geometry and can therefore be highly accurate for detailed stress analysis. These elements automatically adapt to the desired accuracy level. Sparse matrix numerical methods, incorporated in every analysis type, greatly increase the solution speed and reduce the amount of disk space, making numerical processing fast and efficient.

In addition, MSC.NASTRAN features state-of-the-art solution algorithms and procedures including the industry leading sparse matrix solver for fast, accurate solutions. This speed means that more design alternatives can be explored in any given period of time.

 

Key Features

Analysis Types

  • Linear statics
  • Linear statics with inertia relief
  • Normal modes
  • Buckling
  • Design sensitivity-statics
  • Design sensitivity-modes
  • Design sensitivity-buckling
  • Model checkout

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Material Models

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Element Library

Element Type Element Name Description
Scalar ELAS
MASS
Scalar spring (several variations)
Scalar Mass (several variations)
1D BAR
BEAM

BEND
ROD, CONROD
TUBE
Simple beam element
Complex beam element including shear center offset and variable cross section
Curved beam, pipe, or elbow
Rod element
Tension-compression-torsion element
2D QUAD4
QUAD8
QUADR
SHEAR
TRIA3
TRIA6
TRIAR
Quadrilateral plate with membrane-bending or plane strain behavior
Higher-order quadrilateral shell element
Quadrilateral membrane or shell
Shear panel
Triangular plate with membraine-bending or plain strain behavior
Higher-order triangular shell element
Triangular membrane or shell
3D HEXA
PENTA
TETRA
Six-sided solid element with 8-20 grid points
Five-sided solid element with 6-15 grid points
Four-sided solid element with 4-10 grid points
Rigid RBAR
RBE1
RBE2

RROD
RTRPLT
Rigid bar element
Rigid body connected to an arbitrary number of grid points
Rigid body with independent DOFs at a grid point and dependent DOFs at an arbitrary number of grid points
Pin-ended rigid rod
Rigid triangular plate
Interpolation RBE3

RSPLINE
Defines the motion of a reference point as the weighted average of the motions at a set of other grid points
Multipoint constraints for the interpolation of displacements at grid points
Composites BEAM
QUAD4
QUAD8
TRIA3
TRIA6
Complex beam element
Quadrilateral plate
Higher-order quadrilateral plate
Triangular plate
Higher order triangular plate
p-Elements HEXA
PENTA
TETRA
Six-sided solid element with 8-20 grid points
Five sided solid element with 6-15 grid points
Four-sided solid element with 4-10 grid points
Axisymmetric CONEAX
TRIAX6
Conical shell
Triangular cross section ring
Crack Tip CRAC2D
CRAC3D
Two-dimensional crack tip element
Three-dimensional crack tip element
General CONM1
CONM2
DMI
GENEL
6-by-6 symmetric mass matrix
Concentrated mass with offsets
Direct matrix input
General element

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Load Types

Load Type Load Name Description
Point FORCE
MOMENT
Concentrated force (several variations)
Concentrated moment (several variations)
Curve GMLOAD
PLOAD1
Load distributed along a geometric curve
Concentrated, uniform, or linear load applied to 1D elements
Surface GMLOAD
PLOAD
Load distributed along a geometric surface
Pressure load applied to 2D elements or the face of 3D elements (several variations)
Volume GRAV
RFORCE
Steady-state acceleration vectors
Angular velocity or acceleration
Enforced Motion GMBC
GMSPC
SPC
Enforced displacements for geometry (curves and surfaces)
Constraints applied to geometry
Constraints applied to grid points (several variations)
Thermal TEMP
TEMPP1
TEMPRB
Temperatures applied to grid points (several variations)
2D element temperature field
1D element temperature field
Axisymmetric FORCEAX
MOMAX
PLOAD1X
PRESAX
SPCAX
TEMPAX
Concentrated force
Concentrated moment
Surface traction
Pressure loading
Constraints
Applied temperatures
General DMI Direct matrix input
Combination LOAD Combines load sets

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System Requirements

Vendor Model Processor Operating System
Compaq Alpha EV-5, EV-4 UNIX 4.0D
     
HP 9000 PA-RISC 1.1
PA-RISC 2.0
V-Class, PA-RISC 2.0
HP-UX 10.20
HP-UX 10.20
HP-UX 11.0
     
IBM RISC System/6000 PowerClassic, Power2

AIX 4.3.1

     
Intel x86 and compatibles 386+ Windows NT 3.5, 4.0
     
Intel 386+ Linux 2.0.36
     
Silicon Graphics R4K, R5K
R8K, R10K
IRIX 6.2, 6.5
IRIX64 6.4, 6.5
     
Sun SPARC SuperSPARC
UltraSPARC

Solaris 2.5.1, 2.6, 7
Solaris 2.5.1, 2.6, 7

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