Aerothermoelastic Analisys of a FGM wing
Aerothermoelastic Analisys of a FGM wing
(OP)
I'm going to analyze the aerothermoelastic behaviour of a wing made of Functionally Gradient Material (FGM).
Does anyone already done such a thing?
Could you give some tips, or tell me where to find some articles?
Does anyone already done such a thing?
Could you give some tips, or tell me where to find some articles?




