Low Pressure Turbine T106A Transition Modelling

  1. We have used Fluent 14.5
  2. Solver is coupled pressure based
  3. Flow scheme is 2nd order accurate
  4. Time scheme is also 2nd order accurate
  5. Meshing was done in Gambit. Mesh is hybrid. Mesh in boundary layer is map and in the rest of domain is triangular
  6. Two meshes are used: Baseline and fine
  7. Time step is 0.001, 0.0001 and 0.00001
  8. Total simulation time is 0.1 second and data is averaged over all time steps.

ImageImage

Image

Image

Image

Image

Image

Advertisements