Abstract
The utility of boundary layer fences in 90° turning ducts and turbine passages is investigated. The present study isolates the passage vortex structure from the horseshoe vortex by using a duct flow rather than a turbine cascade. The turbine passage or internal coolant duct is simulated to study the interaction effects of the boundary layer fence and the passage flow dominated by the passage vortices.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 83-99 |
| Number of pages | 17 |
| Journal | American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD |
| Volume | 300 |
| State | Published - 1994 |
| Event | Proceedings of the 1994 International Mechanical Engineering Congress and Exposition - Chicago, IL, USA Duration: Nov 6 1994 → Nov 11 1994 |
All Science Journal Classification (ASJC) codes
- Mechanical Engineering
- Fluid Flow and Transfer Processes