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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

27th May 2015
Each student submits two copies of Final report plus an extra copy of their technical abstract, plus their log book or electronic equivalent to Group Centres by 4pm.


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