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LES Modelling of Turbine Blade Trailing Edges

Professor Paul Tucker

In this project the LES modelling of the wall type jets issuing from the trailing edges of turbine blades will be explored using a range of LES techniques. Linear and non-linear LES models will be considered along with HYBRID implicit LES-RANS techniques.

4th Year Project Deadlines

Wednesday, 28th May 2014. Last day for handing in final reports to group centres.  Each student submits 2 copies plus an extra copy of their technical abstract, plus their log book or CD of electronic equivalent

Thursday, 29th May, Friday 30th May.  Group A project presentations, Hopkinson Laboratory, Hopkinson West Meeting Room and Whittle Laboratory.


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