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Problem Specification
A NACA0012 Airfoil is supported such that one end is fixed at a wall and the end is free. The airfoil has a chord of 1 meter, a span of 5 meters, and a thickness of 0.01 meters. The airfoil is Aluminum 6061-T6. Find the first 6 modes of vibration of the airfoil using ANSYS Workbench.
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