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Strain gauge position based on FEM?

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Ionut Cosmin

Aerospace
Joined
Jul 22, 2016
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24
Location
RO
Hi all, I am trying to determine the best position for strain gauges on a milled aluminum aviation part that will be tested. I am checking the max principal strains in the FE model and I am wondering if there are any rules, guidelines, or best practices when looking over the FEA and determining the correct spots?
 
on panels, use rosettes. on axial members use single channel s/g.

don't place s/g in a region of high stress gradient.

another day in paradise, or is paradise one day closer ?
 
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