Design Analysis

Project Title Here

# Created by

Author: |
Department: |
Created Date: | 1/13/2014

# Reviewed by

Reviewer: |
Department: |
Model Created Date: | 1/13/2014
Reviewer Comments: |

# Executive Summary

This is where to put your Executive summary. So, replace this text with your overall Project Description.

# Summary

## Model Information

Analysis Type - Transient Stress (Direct Integration)
Units - Custom - (N, mm, s, °C, K, V, ohm, A, J)
Model location - D:\Autodesk Simulation Manuscript\c10_Autodesk-Simulation\new-tut01\Part1.fem
Design scenario description - Design Scenario # 3

# Analysis Parameters Information

## Processor Information

Number of time steps | 80
Time Step Size | 0.05 s
Output interval | 1
Damping Alpha | 0.01
Damping Beta | 0.01
Dynamic Nodal Load 1 - Node Number | 1
Dynamic Nodal Load 1 - Load Curve | 1
Dynamic Nodal Load 1 - Type | Translation
Dynamic Nodal Load 1 - X Scale | 0
Dynamic Nodal Load 1 - Y Scale | 0
Dynamic Nodal Load 1 - Z Scale | 0
Dynamic Nodal Load 1 - Activation Time | 0
Disable Calculation and Output of Strains | No
Avoid Bandwidth Minimization | No
Stop After Stiffness Calculations | No
Ground Motion Type | None
Stress Data in Output File | No
Equation Numbers Data in Output File | No
Element Input Data in Output File | No
Nodal Input Data in Output File | No
Nodal Printout Type Indicator | Histories and Maxima

# Part Information

Part ID | Part Name | Element Type | Material Name
--- | --- | --- | ---
1 | Part1 | Brick | Stainless Steel (AISI 202)

# Element Information

### Element Properties used for:

- Part1

Element Type | Brick
Compatibility | Not Enforced
Integration Order | 2nd Order
Stress Free Reference Temperature | 0 °C

# Material Information

###
Stainless Steel (AISI 202) -Brick

Material Model | Standard
Material Source | Autodesk Simulation Material Library
Material Source File | C:\Program Files\Autodesk\Simulation 2014\matlibs\algormat.mlb
Date Last Updated | 2012/07/12-16:46:54
Material Description | Annealed
Mass Density | 7.85476108852978e-006 kg/mm³
Modulus of Elasticity | 206842.718782938 N/mm²
Poisson's Ratio | 0.3
Thermal Coefficient of Expansion | 1.566e-005 1/°C
Yield Strength | 310.264078174406 N/mm²
Ultimate Strength | 655.001942812636 N/mm²

# Loads

### FEA Object Group 4: Nodal Forces

#### Nodal Force

ID | Description | Vertex Number | Node Number | Magnitude (N) | Vx | Vy | Vz | Load Case / Load Curve
--- | --- | --- | --- | --- | --- | --- | --- | ---
1 | Unnamed | 2 | 2 | -200.000000 | 0.000000 | 1.000000 | 0.000000 | 1
5 | Unnamed | 11 | 11 | -200.000000 | 0.000000 | 1.000000 | 0.000000 | 1
2 | Unnamed | 3 | 3 | -200.000000 | 0.000000 | 1.000000 | 0.000000 | 1
4 | Unnamed | 10 | 10 | -200.000000 | 0.000000 | 1.000000 | 0.000000 | 1
3 | Unnamed | 9 | 9 | -200.000000 | 0.000000 | 1.000000 | 0.000000 | 1

# Constraints

### FEA Object Group 3: Surface General Constraints

#### Surface General Constraint

ID | Description | Part Number | Surface Number | Tx | Ty | Tz | Rx | Ry | Rz
--- | --- | --- | --- | --- | --- | --- | --- | --- | ---
3 | Unnamed | 1 | 3 | Yes | Yes | Yes | Yes | Yes | Yes

# Results Presentation Images

## Displacement

## Stress