Integrated Aeroelasticity Analysis for Turbomachinery (European and Asian business hours)
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
Session 1 - European and Asian business hours: click here to register
9:00AM (Brussels), 3:00PM (Beijing), 4:00PM (Tokyo)
Please ensure you register at least 24 hours in advance. All registrants must state a professional or company affiliation.
Contact email@example.com if you have any questions.
PC-based attendees: Windows® 7, Vista, XP or 2003 Server
Macintosh®-based attendees: Mac OS® X 10.5 or newer