Design Analysis

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# Created by

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Created Date: | 1/13/2014

# Reviewed by

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Model Created Date: | 1/13/2014
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# Executive Summary

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# Summary

## Model Information

Analysis Type - MES with Nonlinear Material Models
Units - Custom - (N, mm, s, °C, K, V, ohm, A, J)
Model location - D:\Autodesk Simulation Manuscript\c10_Autodesk-Simulation\new-tut01\c10_tut05.fem
Design scenario description - Design Scenario # 4

# Analysis Parameters Information

## Event Information

Number of interval zones = 1

Time Zone Index | Duration (s) | Number of time steps
--- | --- | ---
1 | 8 | 80

## Gravity Information

Acceleration Due To Body Force = 0 mm/s²

Load Curve Number for Gravity Load = 1

Acceleration/Gravity X Multiplier | Acceleration/Gravity Y Multiplier | Acceleration/Gravity Z Multiplier
--- | --- | ---
0 | 0 | -1

## Centrifugal Information

Angular Velocity (Omega) Magnitude = 0 (RPM)

Load Curve Multiplier = 1

Load Curve Number = 1

| X | Y | Z
--- | --- | --- | ---
Rotation Center Point (mm) | 0 | 0 | 0
Rotation Axis | 0 | 0 | 0

Angular Acceleration (Alpha) Magnitude = 0 (RPM/s)

Load Curve Multiplier = 1

Load Curve Number = 1

| X | Y | Z
--- | --- | --- | ---
Rotation Center Point (mm) | 0 | 0 | 0
Rotation Axis | 0 | 0 | 0

## Load Curve Information

#### Load Curve 1: Load Curve

Time (s) | Multiplier
--- | ---
0 | 0
1 | 1
2 | 1
3 | 1.5
4 | 2
5 | 2.5
6 | 2.5
7 | 3
8 | 3

## Multiphysics Information

Default Nodal Temperature | 0 °C

## Processor Information

Analysis Type | Fully Manual
Type of Shell Pressure Loading | None
Load Curve Number for Shell Pressure Loads |
Smooth Shell Pressure | No
Hydrostatic Pressure Control for Shell Elements | None
Z Coordinate Datum for Hydrostatic Pressure | mm
Weight Density of Fluid Causing Shell Hydrostatic Pressure | N/mm³
Nodal Temperature Time-Variation Load Curve Index | 1
Where On Disk Is Nodal Temperature Data Stored | No thermal Data
Temperature Data File | None
Output Results of All Time Steps | No
Output Results of All Time Steps With Wall Interaction | No
Calculate and Output Strains | No
Output Reaction Forces | Calculated
Number of time steps |
Initial Time Step Size | 0.05 s
Nonlinear Iterative Solution Method | Unknown Value
Maximum Number of Iterations | 15
Convergence Criteria | Displacement
Displacement Tolerance | 0.0001
Force Tolerance | 1e-015
Line Search Convergence Tolerance | 0.5
Number of Time Steps Between Iterations | 1
Number of Time Steps Between Reforming Stiffness Matrix | 1
Time Integration Methods Suggested for Type of Analysis | General: MES, NLS
Parameter for MES Integration Method | 1
First Parameter for LS Integration Method | 0.5
Second Parameter for LS Integration Method | 0.25
Output interval | 1
Starting Time for Event | 0 s
Interval to save restart data. | Last step only.
Resume from Step | 0
Resume/Extend Run | No
Time Step Number Extension | 0
Use A Constant Time Step Size | No
Decrease Trigger: Rate of convergence | Unknown Value
Decrease Trigger: Allow for Non-monotonic convergence | Yes
Decrease Trigger: High Solution Tolerance | Yes
Time Step Change Factor | 2
Increase Trigger: Number of Convergent Time Steps | 4
Increase Trigger: Increment to Number of Convergent Time Steps | 4
Time step reduction if there are distorted elements | Yes
Apply Rayleigh Damping | No
Mass-related Rayleigh Damping Coeeficient | 0.05
Stiffness-related Rayleigh Damping Coefficient | 0.05
Time Step Data In Output File | No
Equation Numbers Data in Output File | No
Element Stiffness In Output File | No
Global Stiffness In Output File | No
Displacement of Nodes In Output File | No
Velocity of Nodes In Output File | No
Acceleration of Nodes In Output File | No
Element Input Data in Output File | No
Nodal Input Data in Output File | No
Initial Condition Input Data In Output File | No
Printout Blocks Output To File | No
Mass Representation | Lumped
Matrix Reform Interval Within Each Time Step | 1
Maximum Stiffness Reformations Per Interval | 1
Number of Time Steps Between Reforming Stiffness Matrix | 1
Avoid Bandwidth Optimization | No
Bandwidth Optimization Method | Single Body
Convergence tolerance | 1e-006
Maximum Number of Iterations | 1000
Number of processors | -1
Run Static Analysis | No
Type of Solver | Automatic
Tolerance for stiffness matrix entries | 0

# 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
Material Model | Isotropic
Midside Nodes | Not Included
Orthotropic Material Principle Axis | X-direction
Material Axis Rotation Angle | 0 °
Analysis Formulation | Total Lagrangian
Compatibility | Not Enforced
1st Integration Order | Unknown Value
2nd Integration Order | Unknown Value
Allow for overlapping elements | No
Selective Reduced Integration (mean-dilation) | No

# 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
Damping | 0 s

# Loads

### FEA Object Group 4: Nodal Forces

#### Nodal Force

ID | Description | Vertex Number | Node Number | Magnitude (N) | Vx | Vy | Vz | Load Case / Load Curve
--- | --- | --- | --- | --- | --- | --- | --- | ---
4 | Unnamed | 10 | 10 | -4000.000000 | 0.000000 | 1.000000 | 0.000000 | 1
3 | Unnamed | 9 | 9 | -4000.000000 | 0.000000 | 1.000000 | 0.000000 | 1
5 | Unnamed | 11 | 11 | -4000.000000 | 0.000000 | 1.000000 | 0.000000 | 1
2 | Unnamed | 3 | 3 | -4000.000000 | 0.000000 | 1.000000 | 0.000000 | 1
1 | Unnamed | 2 | 2 | -4000.000000 | 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

No Results Images available.