The viscous, Navier-Stokes solver for turbomachinery applications,
MSUTC has been modified to include the rotating frame formulation.
The three-dimensional thin-layer Navier-Stokes equations have been
cast in a rotating Cartesian frame enabling the freezing of grid
motion. This also allows the flow-field associated with an isolated
rotor to be viewed as a steady-state problem. Consequently, local
time stepping can be used to accelerate convergence. The
formulation is validated by running NASA's Rotor 67 as the test
case. results are compared between the rotating frame code and the
absolute frame code. The use of the rotating frame approach greatly
enhances the performance of the code with respect to savings in
computing time, without degradation of the solution.
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