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Aeroelastic analysis of a rotor blade


Hi guys,

i'm new to Femap and i'm trying to learn about the aeroelastic module. I found a good webinar from aerostructure that explained a litte about the argument, however when trying to do the same for a rotor blade i got stuck. 


So my problem is actually how to model a rotating blade, and pass the information to a sol 146 analysis. 


Anotther problem woul be the aerodynamic model...shoudl i give him a rotational velocity?


Thanks for your attention...if possible even directing me to some webinar about rotating blade would be appreciated.