Abstract:
The simulation of turbulent flow of
viscous compressible fluid in the cone cavity of a high pressure
turbine is considered. The Reynolds-averaged Navier–Stokes
equations and the equations of the Spalart–Allmaras turbulence model are used in
computations. The numerical results based
on the two-dimensional (axisymmetric model) formulation of the problem and
based on the three-dimensional (model in the form of a sector with periodic boundary
conditions in the circumferential direction) formulation of the problem are compared.
Some small 3D details of the model, such as bolts and flanges, and their influence
on the flowfield are taken into account in the computational model.
The flow structure (distributions of flow quantities,
location and number of recirculation regions, flow direction) obtained in the cavity
for various models is compared.
Keywords:drive cone cavity; gas turbine; turbulence; compressibility; rotation.