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.
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 |