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 - 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)	Vy	Load Case / Load Curve
4	Unnamed	10	10	-4000.000000	1.000000	1
3	Unnamed	9	9	-4000.000000	1.000000	1
5	Unnamed	11	11	-4000.000000	1.000000	1
2	Unnamed	3	3	-4000.000000	1.000000	1
1	Unnamed	2	2	-4000.000000	1.000000	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.

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