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{color:#ff0000}{*}Problem Specification{*}{color}
[1. Pre-Analysis & Start-Up|ANSYS 12 - Cantilever Beam Modal Analysis - Pre-Analysis & Start-Up]
[2. Geometry|ANSYS 12 - Cantilever Beam Modal Analysis - Geometry]
[3. Mesh|ANSYS 12 - Cantilever Beam Modal Analysis - Mesh]
[4. Setup (Physics)|ANSYS 12 - Cantilever Beam Modal Analysis - Setup (Physics)]
[5. Solution|ANSYS 12 - Cantilever Beam Modal Analysis - Solution]
[6. Results|ANSYS 12 - Cantilever Beam Modal Analysis - Results]
[7. Verification and Validation|ANSYS 12 - Cantilever Beam Modal Analysis - Verification & Validation]
[Exercises|ANSYS 12 - Cantilever Beam Modal Analysis - Exercises]
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{note|title=blahblah}Prior, to attempting this tutorial, you must complete the [Cantilever Beam Tutorial|ANSYS 12 - Cantilever Beam - Problem Specification] .  If you have not yet completed the [Cantilever Beam Tutorial|ANSYS 12 - Cantilever Beam - Problem Specification], please do so now.{note}

h2. Problem Specification

Consider an aluminum beam that is clamped at one end, with the following dimensions.

|| Length | 4 m ||
|| Width | 0.346 m ||
|| Height | 0.346 m ||

The aluminum used for the beam has the following material properties.

|| Density | 2,700 kg/m^3 ||
|| Youngs Modulus | 70x10^9 Pa ||
|| Poisson Ratio | 0.35 ||
Using ANSYS Workbench find the first six natural frequencies of the beam.
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