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2G loading on UAV wing

    • twnspl


      I am trying to simulate a simple wing in ansys structural. I have obtianed the pressure loading from CFD analysis (OpenFOAM). However I want to see the behaviour of the wing in different g loading. That is 2g and 3g load cases, how do I go about simulating these scenarios ? I tried applying acceleration condition with 9.81m/s^2 and then increasing this value but I don't get any difference in deflection, stress, etc.

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