Date: Wed, 29 Jun 2022 01:17:52 -0500 (CDT) Message-ID: <1835531195.12203.1656483472639@cornell1-cos-conf1.managed.contegix.com> Subject: Exported From Confluence MIME-Version: 1.0 Content-Type: multipart/related; boundary="----=_Part_12202_806792632.1656483472638" ------=_Part_12202_806792632.1656483472638 Content-Type: text/html; charset=UTF-8 Content-Transfer-Encoding: quoted-printable Content-Location: file:///C:/exported.html ANSYS - Cantilever Beam Modal Analysis

# ANSYS - Cantilever Beam Modal Analysis

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Author: John Singleton, Cornell University

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Important Note

Prior, to attempting this tutorial, you must complete the Cantilever Beam Tutorial. The= Cantilever Beam Tutorial covers the static structural analysis for th= e same geometry. If you have not yet completed the Cantilever Beam Tutorial= , please do so now.

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# Can= tilever Beam Modal Analysis

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Created using ANSYS 13.0

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## Problem Sp= ecification

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

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 Length 4 m 0.346 m 0.346 m
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The aluminum used for the beam has the following material properties.=20

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 Density 2,700 kg/m^3 70x10^9 Pa 0.35
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Using ANSYS Workbench find the first six natural frequencies of the beam= and the mode shapes.

Go to Step 1: Pre-Analysis & Start-up

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Go to all ANSYS L= earning Modules

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