Characterization of Ingestion through the Rim Seal of Rotor-Stator Disk Cavity in a Subscale Single-Stage Axial Turbine
abstract: In order to achieve higher gas turbine efficiency, the main gas temperature at turbine inlet has been steadily increased from approximately 900°C to about 1500°C over the last few decades. This temperature is higher than the maximum acceptable temperature for turbine intern...
| Other Authors: | |
|---|---|
| Format: | Dissertation |
| Language: | English |
| Published: |
2014
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/2286/R.I.25947 |