The CFD analysis accounts for the elastic deformations using a dynamically deforming mesh system. All the rotor blades are assumed to be identical, therefore to reduce the computational complexity the CFD calculations are performed for a single blade. This accounts for the near wake flow field. But the far wake effects because of the trailed tip vortices from all the blades have to be included separately.
Author:-Sitaraman, Jayanarayanan
Source:- DRUM
URL: http://hdl.handle.net/1903/310
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