Quote:
Originally Posted by tim-tim
When you ask how strong or what the strength of something is, please provide more details in the application (i.e. bending, tension, compression, fatigue, fasteners, etc)
Some have mentioned typical alloys 5052-H34, 6061-T6, 7075-T6. In addition to these 5052-H32 and 2024-T3. This list contains the alloys that are (typically) used and kept in stock at the aircraft modification shop that i work at.
Also, is it extremely important to find a sheet of aluminum that is 0.06275"? The fractional size of 1/16th (0.0625") is usually sold as 0.063". Please inquire if you have any other questions. Sheet metal design can be very useful, IF you know how and where to use it.
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I'm sorry that I can't be detailed on the application, but the impulse on lets say just this 1/16th of an inch thick aluminum shape is ~4.5 Kg m/s of compression. The only other force would be an optional fastener (servo screw more than likely) that doesn't support anything. Also, this wouldn't be flat bought, but rather manufactured so beginning size isn't that big of an issue.