Online
Venue Details »
- 13th April 2021
3:00 pm - 3:15 pm
13 April 2021
10 AM EDT / 3 PM BST/ 7:30 PM IST
The flow within a gas turbine blade is very complex with the blade passage film and internal cooling passages. The ability to simulate these types of flows has been limited by the mesh and models available. With the new features and capabilities in Ansys CFD, modeling of film cooling holes, cooling tree and passages can be modeled with different levels of fidelity.
- Injection regions for modeling film cooling flows, without meshing holes explicitly
- Efficient, rapid mesh generation for fully resolved and meshed cooling flow passages
- Full conjugate heat transfer with rapid solution methods
Registration / Further Information
Simply choose one of the following options to receive further information or to register.
- Complete the form opposite
- Call us on +44 (0)161 474 6886
- Email us at events@WildeAnalysis.co.uk
Please note that this event is free to attend but registration is essential.
Location
Venue: Online
Address:
Online
Description:
Details on how to join the webinar will be emailed to you once registered.
- Injection regions for modeling film cooling flows, without meshing holes explicitly
- Efficient, rapid mesh generation for fully resolved and meshed cooling flow passages
- Full conjugate heat transfer with rapid solution methods