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With these two questions answered, I can determine how many two-clamp fasteners are needed to support the load of the aerobody. To be clear, since each clamp has two bolts, the amount of load the system can hold is both bolts totaled.
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Misc notes:
Could also FEA the entire body to determine the positioning of the fasteners, but it's not that accurate.If there are two bolts for every clamp, does this mean each bolt will provide a given frictional force, or is it total?