Quote:
Originally Posted by baronep
Our sheetmetal guys say that they can produce .125, .1 and .080 thicknesses of 5052 alloy. Strength-wise, which thickness would be optimal? How would creating cutouts affect the weight/strength ratio?
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To answer your question, there is no 'correct' answer. The material should be selected based on application of the component being designed and what you (the designer) are asking the component to do.
Yes, typically teams do use .090 thk material for chassis construction. Is there a reason? I suppose that few (if any) have completed a structural analysis on the frame and all of the interaction associated. There are many types of 'quick calculations' that can be made, but these really won't be quick and will actually be a simplified representation of the actual frame.
I know I have not offered a lot of direct insight, so let me do that now:
5052 is a softer aluminum alloy, which is great for bending components because a tight radius can be held (making it almost a point). The con, it bends easy and does not have the strength of other alloys. In order from 'weaker' to 'stronger' alloys 5052, 6061, 2024, 7075. There are more alloys out there than this, but these are the most commonly used. The best part, they all have roughly the same density. Going with the 'stronger' materials will mean a larger bend radius is required for the part. ***IF you have mentors with an engineering background (or you want to learn yourself) you can design for thinner materials in places by switching materials.***
If you are welding it gets a bit more tricky, 5052 and 6061 are the alloys you want to stick with. Just another tidbit, be careful on the use of terms such as optimal.
Hope this helps, and let me know if you have any other questions, or need more clarification on certain items. It is early in the morning, and I apologize for the lost train of thoughts at times.