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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

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