Influence of spanwise and streamwise film hole spacing on adiabatic film effectiveness for effusion-cooled gas turbine blades
To meet the challenges of increased thermal loads and performance demands on aeroengine turbine blades, more advanced cooling techniques are required. This study used a modification of the well-known Goldstein equation to predict film effectiveness for an individual film cooling hole and applied the...
| Main Authors: | , , , , |
|---|---|
| Format: | Journal article |
| Language: | English |
| Published: |
MDPI
2021
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