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Design Analysis

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Created Date:
2012-10-22

Reviewed by

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Model Created Date:
2012-10-22
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Executive Summary


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Summary

Model Information

Analysis Type - Static Stress with Linear Material Models
Units - Custom - (kN, m, s, °C, K, V, ohm, A, J)
Model location - C:\Users\JPS\Documents\Algor\Rama4.fem
Design scenario description - Design Scenario # 1

Analysis Parameters Information

Load Case Multipliers


Static Stress with Linear Material Models may have multiple load cases. This allows a model to be analyzed with multiple loads while solving the equations a single time. The following is a list of load case multipliers that were analyzed with this model.

Load Case Pressure/Surface Forces Gravity/Acceleration Angular Velocity (Omega) Angular Acceleration (Alpha) Displacement Thermal Electrical
1 1 1 0 0 1 0 0

Gravity Information


The following lists the values used if acceleration or gravity was included in the analysis. The Acceleration/Gravity direction multiplier is multiplied by the Acceleration Due To Body Force which is then multiplied by the Acceleration/Gravity load case multiplier.

Acceleration Due To Body Force = 9 m/s²

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

Multiphysics Information


Default Nodal Temperature 0 °C
Source of Initial Nodal Temperatures Model file  
Time step from Heat Transfer Analysis Last  
Default nodal voltage 0 V
Source of nodal voltages Model file  

Processor Information


Type of Solver Automatic  
Disable Calculation and Output of Strains No  
Calculate Reaction Forces Yes  
Invoke Banded Solver Yes  
Avoid Bandwidth Minimization No  
Stop After Stiffness Calculations No  
Displacement Data in Output File No  
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  
Centrifugal Load Data in Output File No  

Part Information

Part ID Part Name Element Type Material Name
1 Rama stalowa Beam AISI E 52100 Steel

Element Information

Element Properties used for:

Element Type Beam
Stress Free Reference Temperature 0 °C
Layer 1 - Area 0  
Layer 1 - SA2 0  
Layer 1 - SA3 0  
Layer 1 - J1 3  
Layer 1 - I2 1  
Layer 1 - I3 0  
Layer 1 - S2 0  
Layer 1 - S3 0  
Layer 2 - Area 0  
Layer 2 - SA2 0  
Layer 2 - SA3 0  
Layer 2 - J1 3  
Layer 2 - I2 1  
Layer 2 - I3 0  
Layer 2 - S2 0  
Layer 2 - S3 0  
Layer 3 - Area 0  
Layer 3 - SA2 0  
Layer 3 - SA3 0  
Layer 3 - J1 1  
Layer 3 - I2 8  
Layer 3 - I3 9  
Layer 3 - S2 0  
Layer 3 - S3 0  
Layer 4 - Area 0  
Layer 4 - SA2 0  
Layer 4 - SA3 0  
Layer 4 - J1 1  
Layer 4 - I2 8  
Layer 4 - I3 0  
Layer 4 - S2 9  
Layer 4 - S3 0  
Layer 5 - Area 0  
Layer 5 - SA2 0  
Layer 5 - SA3 0  
Layer 5 - J1 2  
Layer 5 - I2 9  
Layer 5 - I3 2  
Layer 5 - S2 1  
Layer 5 - S3 0  
Layer 6 - Area 0  
Layer 6 - SA2 0  
Layer 6 - SA3 0  
Layer 6 - J1 2  
Layer 6 - I2 9  
Layer 6 - I3 2  
Layer 6 - S2 1  
Layer 6 - S3 0  
Layer 7 - Area 0  
Layer 7 - SA2 0  
Layer 7 - SA3 0  
Layer 7 - J1 1  
Layer 7 - I2 8  
Layer 7 - I3 9  
Layer 7 - S2 0  
Layer 7 - S3 0  

Material Information



AISI E 52100 Steel -Beam

Material Model Standard  
Material Source Autodesk Simulation Material Library  
Material Source File C:\Program Files\Autodesk\Simulation 2013\matlibs\algormat.mlb  
Date Last Updated 2004/10/28-16:02:00  
Material Description None  
Mass Density 7 kN·s²/m/m³
Modulus of Elasticity 210000000 kN/m²
Poisson's Ratio 0.3  
Thermal Coefficient of Expansion 0 1/°C

Loads

FEA Object Group 3: Beam Distributed Loads

Beam Distributed Load

IDDescriptionLine IDElement IDMagnitude-I (N/m)Vx-IVy-IVz-IMagnitude-J (N/m)Vx-JVy-JVz-JAB
1Unnamed50375,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
2Unnamed51385,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
3Unnamed52395,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
4Unnamed53405,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
5Unnamed54415,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
6Unnamed55425,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
7Unnamed56435,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000
8Unnamed57445,0000000,0000000,000000-1,0000005,0000000,0000000,000000-1,0000000,0000001,000000

FEA Object Group 4: Nodal Forces

Nodal Force

IDDescriptionVertex NumberNode NumberMagnitude (kN)VxVyVzLoad Case / Load Curve
1Unnamed783120,0000000,0000000,000000-1,0000001
2Unnamed722820,0000000,0000000,000000-1,0000001

FEA Object Group 5: Nodal Forces

Nodal Force

IDDescriptionVertex NumberNode NumberMagnitude (kN)VxVyVzLoad Case / Load Curve
3Unnamed873515,0000000,000000-1,000000-1,0000001
4Unnamed933815,0000000,000000-1,000000-1,0000001

Constraints

FEA Object Group 1: Nodal General Constraints

Nodal General Constraint

IDDescriptionVertex NumberNode NumberTxTyTzRxRyRz
1Unnamed4012YesYesYesNoNoNo
2Unnamed5017YesYesYesNoNoNo

FEA Object Group 2: Nodal General Constraints

Nodal General Constraint

IDDescriptionVertex NumberNode NumberTxTyTzRxRyRz
3Unnamed307YesYesYesYesYesYes
4Unnamed6022YesYesYesYesYesYes

Results Presentation Images

Displacement