Turbo in 15 Minutes: Conjugate Heat Transfer and Blade Film Cooling
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