Integrated Aeroelasticity Analysis for Turbomachinery (European and Asian business hours)

Date
29 JANUARY 2014
Location
Europe

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) 

Another session of this webinar will take place at N./S. American business hours.

Preparation: 

Please ensure you register at least 24 hours in advance.  All registrants must state a professional or company affiliation.

 Contact webinars@numeca.com  if you have any questions. 

System Requirements: 

PC-based attendees:  Windows® 7, Vista, XP or 2003 Server 

Macintosh®-based attendees: Mac OS® X 10.5 or newer