Design Analysis

Project Title Here

# Created by

Author: |
Department: |
Created Date: | 9/25/2013

# Reviewed by

Reviewer: |
Department: |
Model Created Date: | 9/25/2013
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 - Natural Frequency (Modal)
Units - Custom - (N, mm, s, °C, K, V, ohm, A, J)
Model location - D:\Autodesk Simulation Manuscript\c10_Autodesk-Simulation\Tut01\c10_tut01.fem
Design scenario description - Design Scenario # 1

# Analysis Parameters Information

## Processor Information

Number of Frequencies To Calculate | 5
Cutoff Frequency | 0 cycles/s
Frequency Shift | 0 cycles/s
Expected Rigid Body Modes | 1
Maximum Number of Iterations | 32
Number of Vectors in Subspace Iteration | 0
Orthogonality Check Printout | None
Convergence Value for Eigenvalue |
Avoid Sturn Sequence Check | No
Avoid Bandwidth Minimization | No
Stop After Stiffness Calculations | No
Attempt to Run Despite Errors | No
Do Not Save Restart Files | No
Displacement Data in Output File | No
Equation Numbers Data in Output File | No
Matrices in Output File | No
Element Input Data in Output File | No
Nodal Input Data in Output File | No

# Part Information

Part ID | Part Name | Element Type | Material Name
--- | --- | --- | ---
1 | Part 1 | Beam | Stainless Steel (AISI 446)

# Element Information

### Element Properties used for:

- Part 1

Element Type | Beam
Stress Free Reference Temperature | -17.7777777777778 °C
Layer 1 - Area | 100
Layer 1 - SA2 | 84.9600000000002
Layer 1 - SA3 | 84.9600000000002
Layer 1 - J1 | 1408
Layer 1 - I2 | 833.299999999998
Layer 1 - I3 | 833.299999999998
Layer 1 - S2 | 166.7
Layer 1 - S3 | 166.7

# Material Information

###
Stainless Steel (AISI 446) -Beam

Material Model | Standard
Material Source | Autodesk Simulation Material Library
Material Source File | C:\Program Files\Autodesk\Simulation 2014\matlibs\algormat.mlb
Date Last Updated | 2012/07/12-16:51:30
Material Description | Annealed
Mass Density | 7.7994029714961e-006 kg/mm³
Modulus of Elasticity | 199947.961490173 N/mm²
Poisson's Ratio | 0.3
Thermal Coefficient of Expansion | 1.152e-005 1/°C
Yield Strength | 275.790291710583 N/mm²
Ultimate Strength | 517.106796957344 N/mm²

# Loads

Load data was requested, but no loads were detected.

# Constraints

### FEA Object Group 1: Nodal General Constraints

#### Nodal General Constraint

ID | Description | Vertex Number | Node Number | Tx | Ty | Tz | Rx | Ry | Rz
--- | --- | --- | --- | --- | --- | --- | --- | --- | ---
1 | Unnamed | 1 | 1 | Yes | Yes | Yes | Yes | Yes | Yes

# Results Presentation Images

## Displacement