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Unformatted text preview: orientated perpendicular to the maximum tensile stress component. Verify that the thicknesses you specified in M17 will meet the damage tolerance requirement. If they do not, then specify a new value of the thickness that will allow the panel to meet both the strength and the damage tolerance requirements....
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.
- Fall '05