Full Text Available
Note: Clicking the button above will open the full text document at the original institutional repository in a new window.
Determining appropriate loss coefficients for use in the nozzle-model of a stage-by-stage turbine model
A previously developed turbine modelling methodology, requiring minimal blade passage information, produced a customizable turbine stage component. This stage-by-stage turbine nozzlemodel component was derived from the synthesis of classical turbine theory and classical nozzle theory enabling the co...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Thesis |
| Language: | English |
| Published: |
Department of Mechanical Engineering
2020
|
| Subjects: | |
| Tags: |
No Tags, Be the first to tag this record!
|