Aircraft Cooling System. Aeroespacial. 2ª curso

The objective of this project is to present the CFD analysis of a turbine blade cooling system to optimize airflow and achieve the lowest temperature drop possible to avoid melting of the blade.

Three types of models were presented:

  • 2D
  • 3D
  • Advanced 3D model

The CFD analysis will be performed in ANSYS FLUENT.