With increased power and lighter components requirements, 
engineers must take into account aero-elastic effects for 
state-of-the-art turbomachinery analysis. Flutter is a self-
excited and self-sustained aero-elastic instability phenomenon 
that leads to fatigue and damage. Its investigation can be 
carried out by computing the aerodynamic damping of the 
structure.

FINE/Turbo introduces the modal approach, a novel and 
efficient method for fluid structure interaction prediction 
covering cold-to-hot, forced response and flutter analysis. 

Join us for this FREE webinar and discover how you can take 
benefit from the modal approach implemented in FINE/Turbo.

Registration & Timing:
Duration: approx. 30 minutes