Dix options de NEiNastran que d’autres Nastran n’ont pas
 


1.

NEiNastran Editor

2.

Formulations avancées d’élément Coque et d’élément Solide

3.

Eléments linéaires et non-linéaires de Contact Surface/Surface 3D, de Soudure et Glissement Bi-Directionnel

4.

Interpolation de données

5.

Gestion de base de données modale et filtrage modal

6.

Critères avancées de rupture pour les Matériaux Composites

7.

Calcul de Stability Index pour les Structures Sandwich

8.

Eléments de Câble et Coque non-linéaires en tension seule (Tension-Only)

9.

MAC (Modal Assurance Criteria)

10.

Tri de résultats

 

NEiNastran Editor

Fully integrated and customizable Nastran Editor controls program operation and provides results summary data through an easy to use GUI

Full post processing and results query

Tabbed windows to give immediate access to all input and output files

Field markers make manual editing simple and increase productivity dramatically

Complete online documentation and context sensitive help

Permits batch queuing of jobs for sensitivity and configuration trade studies

Special real time controls allow changing solution parameters while running

Real time 2D x-y plotting and 3D deformed shape and contour plotting with optional MS Excel Comma Separated Variable (.CSV) file output

 

     

 
 
 

Advanced Shell and Solid Element Formulations

Higher order internal shape functions

Proprietary technology of Noran Engineering, Inc.

6 DOF/Node CQUADR/CTRIAR element support

Does not require K6ROT or SNORM

Supported in ALL solution modules including nonlinear

Robust results with distorted elements

Faster mesh convergence

Extensive verification and comparison problem set that demonstrate superior accuracy

 

     

 
 

3D Linear and Nonlinear Surface-to-Surface Contact and Linear and Nonlinear Weld and Bi-Directional Slide Surface Contact Element

Allows translation and rotation at the same time

Permits modeling of problems that are not possible with gap or slide line (3D sliding)

Adaptive stiffness update

Allows friction

Quick and simple to setup, no need to align nodes or elements.

Weld and bi-directional slide element options

Provided as part of the core product and not as a costly add-on.

            

 

Weld and Bi-Directional Slide Element

Uses surface contact element

Default element property settings automatically provide adequate penalty stiffness at the weld interface

Adaptive algorithm automatically adjusts penalty values based on surrounding stiffness

Supported in all solutions

Standard MSC CWELD (spot weld) element also available

 

          

 
 

Data Interpolation Feature

2D or 3D interpolation of input, temperature, displacements, forces, moments, and pressure

Allows load transfer across different models / disciplines:

 

Temperatures

-->

Thermal - mechanical coupling

Forces / Moments

-->

EMAG – mechanical coupling

Pressures

-->

CFD – FEM coupling

Displacements

-->

FEM – CFD coupling

Accurate and user-controllable 2D / 3D polynomial interpolation through least-squares approach

Heat Transfer Model                  Structural Model
2982 Elements                         15100 Elements

 

Modal Database Management, and Modal Filtering

Modal Base filtering option based on modal effective mass

Modal Data save and re-use option

Very big savings in CPU time possible with all Modal based response method avoiding re-calculation of modal data

Simple interface: best usability

 

 

Application Workflow Example: DDAM

 
 
 

Advanced Failure Criteria for Composites

LaRC02 Set of Criteria

 

• Developed by NASA

 

• First-ply-failure

 

• Physically based

 

• Hashin, Puck approach

 

• No additional material properties required compared to Tsai-Wu

 

• Failure mode taken into account

 

• Extensive validation (WWFE)

 

 

 

 
 

Stability Index Output for Sandwich Structures

Theory based on Facesheet Wrinkling in Sandwich Structures, NASA-CR-1999-208994, 1999

 

Honeycomb Sandwich Material Properties

 

Material

Modulus of Elasticity (msi)

Tensile Limit (ksi)

Compression Limit (ksi)

Shear Limit (ksi)

Aluminum Face Sheets

10.0

35.0

35.0

23.0

Honeycomb Core

0.1

0.1

0.3

0.2

Bonding Material

-

-

-

0.1

 
 

Honeycomb Sandwich Results Output

 

 
 

Nonlinear Tension-Only Cable Elements

 

• Allows initial slack or preload

 

• Ultimate tensile stress can be specified above which the cable fails

 

• Supports temperature dependent material properties

 

• Supported in all solutions

Nonlinear Tension-Only Shell Element

 

• Tension only membrane reverts to a shear panel in compression

 

• Designed for analyzing semi-monocoque aircraft structures

 

• Controllable compression stiffness scale factor

 

• Currently used by Cessna Aircraft for production design work

 

     

 
 

Modal Assurance Criteria (MAC)

Correlation carried out by NEiNastran in a normal modes analysis

No 3rd party software required

External or test data can be in CSV, DMIG or MDB format

Non-MDB (Modal Database) data will be automatically converted to MDB for re-use

Automatic mapping of test to model grid positions

Interpolation of test eigenvalue shape to model

MAC and ORTHO-MODE correlation supported

Text output in the Model Results Output File

Graphical support is included in the NEiNastran Editor

Future developments include FRF correlation

 

     

 
 

Results Sorting

Automatic and user definable measure sorting for handling multiple load case results

Powerful grid and element set generator for generating sets that can be used to control output, define measure coordinate systems, generate grid point temperatures, and define measure sort commands

 




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