bladesandvanes
Aerospace
Hello, Hopefully someone can help me. I have a compressor blade and have run a modal analysis on it. Is there any way to accurately find the dimesinal location of the max stress to apply a Strain Gauge for Labratory testing. In other words what I am asking is to measure from the base and side to get a true X,Y,Z Location. I know it can be done if you have Design Modeler but can it be done in Classic. I am not real familiar with it but with some advice I should be able to get through it. I solved the Model in Workbench imported it into Classic Solved the model now what? Thanks in Advance. Mike