Tutorial 2: FEA Using Nei Nastran Editor | EML 4500, Study notes of Mechanical Engineering

Material Type: Notes; Professor: Kim; Class: FINITE ELEM ANLYS/DES; Subject: ENGINEERING: MECHANICAL; University: University of Florida; Term: Spring 2009;

Typology: Study notes

Pre 2010

Uploaded on 09/17/2009

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Tutorial 2:
FEA Using Nei Nastran Editor
2
NEi Nastran Editor
So far, we used Nastran FX for pre/post-processing
Input file: 80-column Text file (Tutorial.NAS)
Output file: Text file (Tutorial.OUT) or binary file (Tutorial.O2D)
NEi Nastran Editor
Can generate input text file directly
Need to know formats of input text files
Can easily modify input file for debugging errors
Provide graphical post-processing capability
Nastran FX
Create FE model
NEi Nastran
Solve FE Eq.
Nastran FX
Analyze results
Input
file
Output
file
pf3
pf4

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1

Tutorial 2:

FEA Using Nei Nastran Editor

NEi Nastran Editor

• So far, we used Nastran FX for pre/post-processing

– Input file: 80-column Text file (Tutorial.NAS)

– Output file: Text file (Tutorial.OUT) or binary file (Tutorial.O2D)

• NEi Nastran Editor

– Can generate input text file directly

– Need to know formats of input text files

– Can easily modify input file for debugging errors

– Provide graphical post-processing capability

Nastran FX

Create FE model

NEi Nastran

Solve FE Eq.

Nastran FX

Analyze results

Input

file

Output

file

3

NEi Nastran Editor cont.

Example of Nastran Input File

SOL LINEAR STATIC

DISPLACEMENT(PRINT,PLOT) = ALL

STRESS(PRINT,PLOT,CORNER) = ALL

SPC = 1

LOAD = 1

BEGIN BULK

GRID 1 0 0. 0. 0. 0

GRID 2 0 12. 8. 0. 0

GRID 3 0 12. 0. 0. 0

CBAR 1 1 1 2 1. 0. 0.

CBAR 2 1 2 3 1. 0. 0.

PBAR 1 10.049087 0. 0. 0. 0.

MAT1 1 3.E+7 0. 0. 0.

FORCE 1 2 0 1. 50. 0. 0.

SPC 1 1 123456 0.

SPC 1 3 123456 0.

ENDDATA

Case Control

Bulk Data

Nastran Input File Format cont.

• Define material properties

– MID: material number, E: Young’s modulus, G: shear modulus

– NU: Poisson’s ratio, RHO: density, A: thermal expansion coeff

– TREF: reference temp, GE: structural damping

• Applied Force

– SID: load set number, G: node number, CID: coordinate system

– F: force magnitude, (N1, N2, N3): force direction

• Displacement boundary condition

– SID: displacement BC number, G1, G2: node number

– C1, C2: components, D1, D2: displacement values

– Ex) C1 = 123456 D1 = 0.0 (Fix Ux, Uy, Uz, Rx, Ry, and Rz)

– Ex) C1 = 14 D1 = 0.0 (Fix Ux and Rx)

MAT1 MID E G NU RHO A TREF GE

FORCE SID G CID F N1 N2 N

SPC SID G1 C1 D1 G2 C2 D