Research on Instabilities, Separation and Transition in Three-Dimensional Boundary Layers with Emphasis on Gas-Turbine-Blade Flows
Final rept., 1 Jan 2003-31 Dec 2005
CALIFORNIA UNIV DAVIS DEPT OF MECHANICAL AND AERONAUTICAL ENGINEERING
Pagination or Media Count:
1. Gortler vortices on the concave pressure side of a blade 2. Laminarturbulent transition on the convex side of a blade 3. Turbulent separation under the action of the strong adverse pressure gradient 4. Cooling-film aerodynamics.
- Fluid Mechanics
- Jet and Gas Turbine Engines