Project Details
Description
Three-dimensional endwall contouring in turbines and compressors is a powerful method for
efficiency improvement of modern jet engines. Intensive numerical flow simulations of
highest quality are necessary for the design of 3D endwalls. Therefore a small enterprise and
a university institute will work together to develop the necessary tools and to verify them on
the improvement of an intermediate turbine transition duct.
| Status | Finished |
|---|---|
| Effective start/end date | 1/09/11 → 31/08/15 |
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