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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

Week 7 Start of Mini-conferences

25th November 1.30pm - 6.15pm, Fluids presentations, Hopkinson West Meeting Room.

1st December 1.15 - 5.30pm, Energy Presentations, Hopkinson West Meeting Room.

1st December 1.15 - 5.30pm, Turbo Presentations, Whittle Laboratory

15th January
Submission of Technical Milestone reports to Group Centre (2 copies).


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