Line Post Rev 03-1_rpt
Transcript of Line Post Rev 03-1_rpt
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Design AnalysisProject Title Here
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Created by Author:
Department:
Created Date: 10/8/2013
Reviewed byReviewer:
Department:Model Created
Date:
10/8/2013
Reviewer
Comments:
Executive Summary
This is where to put your Executive summary. So, replace this text with your overall Project Description.
SummaryModel Informat ion
Analysis Type - MES with Nonlinear Material Models
Units - Metric mks (SI) - (N, m, s, °C, K, V, ohm, A, J)
Model location - C:\Users\Marcos\Desktop\UTE\TAREAS\Herrajes mantenimiento\PLANOS CAD\VIEJOS\LINE POST REV 03-1.fem
Design scenario description - Design Scenario # 1
Analysis Parameters Information
Mult iphysics Informat ion
Default Nodal Temperature
0 °C
Processor Informat ion
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Number of interval zones 1
Zone #1 - Duration 1 s
Zone #1 - Number of time steps 20
Analysis Type Fully Manual
Acceleration Due To Body Force 0 m/s²
X Mutiplier 0
Y Mutiplier 0
Z Mutiplier -1
Load Curve Number for Gravity Load 1
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 m
Weight Dens ity of Fluid Caus ing Shell Hydrostatic Pressure N/m³
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
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Initial Time Step Size 0.05 s
Nonlinear Iterative Solution Method Unknown Value
Maximum Number of Iterations 15
Convergence Criteria Displacement
Displacement Tolerance 1e-4
Force Tolerance 1e-15
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 0.50
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: Compressed Elements No
Decrease Trigger: High Solution Tolerance Yes
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Time Step Change Factor 2
Increase Trigger: Number of Convergent Time Steps 4
Increase Trigger: Increment to Number of Convergent Time Steps 4
Apply Rayleigh Damping No
Mass-related Rayleigh Damping Coeeficient 0.05
Stiffness-related Rayleigh Damping Coefficient 0.05
Direction of Centrifugal Load Axis Between Two Points
Centrifugal Load Curve Multiplier 1 m/s²
Centrifugal Rotation RPM
Load Curve Number for Centrifugal Load 1
X Coordinate of First Point of Axis 0 m
Y Coordinate of First Point of Axis 0 m
Z Coordinate of First Point of Axis 0 m
X Coordinate of Second Point on Axis m
Y Coordinate of Second Point on Axis m
Z Coordinate of Second Point on Axis m
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
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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-6
Maximum Number of Iterations 1000
Number of processors -1
Run Static Analysis No
Type of Solver Automatic
Tolerance for stiffness matrix entries 0
Load C urve In format ion
Load Curve 1 TypeTime
Load Curve 1 Index 1 Time 0
Load Curve 1 Index 1 Multiplier 0
Load Curve 1 Index 2 Time 1
Load Curve 1 Index 2 Multiplier 1
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Part InformationPart ID
P ar t N ame E le me nt Ty p e M at er ia l N ame
1 Part 1 Brick Concrete (High Strength)
2 Part 2 Brick Steel (ASTM - A36)
Element InformationElement Properties used for:
· Part 1
· Part 2
Element Type Brick
Material Model Isotropic
Midside Nodes Not Included
Orthotropic Material Principle Axis X-direction
Material Axis Rotation Angle 0 °
Analysis Formulation Total LagrangianCompatibility 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
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Concrete (High Strength) -Brick
Material Model Standard
Material Source Autodesk Simulation Material Library
Material Source File C:\Program Files\Autodesk\Simulation 2013\matlibs\algormat.mlb
Date Last Updated 2004/09/30-16:00:00
Material Description Concrete (high strength)
Mass Density 2351.11693965435 kg/m³
Modulus of Elastic ity 31026407817.4406 N/m²
Poisson's Ratio 0.15
Shear Modulus of Elasticity 0 N/m²
Damping 0 s
Steel (ASTM - A36) -Brick
Material Model Standard
Material Source Autodesk Simulation Material Library
Material Source File C:\Program Files\Autodesk\Simulation 2013\matlibs\algormat.mlb
Date Last Updated 2004/09/30-16:00:00
Material Description Structural Steel
Mass Density 7854.86795748158 kg/m³
Modulus of Elastic ity 199947961490.173 N/m²
Poisson's Ratio 0.29
Shear Modulus of Elasticity 77221281678.9633 N/m²
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Damping 0 s
LoadsFEA Object Group 4: Surface ForcesSurface Force
I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
1 Unnamed 2 62 10000.000000 -0.940806 0.338945 0.000000 Yes 1
FEA Object Group 5: Surface ForcesSurface Force
I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
2 Unnamed 2 58 10000.000000 -0.940806 0.338945 0.000000 Yes 1
FEA Object Group 6: Surface ForcesSurface Force
I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
3 Unnamed 2 5 10000.000000 -0.940806 -0.338945 0.000000 Yes 1
FEA Object Group 7: Surface ForcesSurface Force
I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
4 Unnamed 2 11 10000.000000 -0.940806 -0.338945 0.000000 Yes 1
FEA Object Group 8: Surface ForcesSurface Force
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I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
5 Unnamed 2 48 -534.000000 0.000000 0.000000 1.000000 No 1
FEA Object Group 9: Surface ForcesSurface Force
I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
6 Unnamed 2 52 1568.000000 1.000000 0.000000 0.000000 Yes 1
FEA Object Group 10: Surface ForcesSurface Force
I
D
Descriptio
n
Part
Number
Surface
NumberMagnitude Vx Vy Vz
Follows Moving
Surface
Load Case / Load
Curve
7 Unnamed 2 49 588.000000 0.000000 1.000000 0.000000 Yes 1
Constraints
FEA Object Group 1: Surface General Con straintsSurface General Constraint
I
D
Descriptio
n
Part
Number
Surface
NumberTx Ty Tz Rx Ry Rz
1 Unnamed 1 2 Yes Yes Yes Yes Yes Yes
FEA Object Group 2: Surface General Con straintsSurface General Constraint
I
D
Descriptio
n
Part
Number
Surface
NumberTx Ty Tz Rx Ry Rz
2 Unnamed 1 3 Yes Yes Yes Yes Yes Yes
FEA Object Group 3: Surface General Con straints
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Surface General Constraint
I
D
Descriptio
n
Part
Number
Surface
NumberTx Ty Tz Rx Ry Rz
3 Unnamed 1 1 Yes Yes Yes Yes Yes Yes
Results Presentation Images
Disp lacement