Numerical investigation on vane leading edge impingement cooling performance under influences of ribs established between adjacent jets
Numerical studies on the vane leading edge jet impingement cooling are conducted to analyzed the influence of the cylindrical ribs applied between adjacent jets. A one-way inlet coolant supply channel and a one-way exit semicircular target channel are connected through single array of 10 jet holes....
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2024-11-01
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| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1177/16878132241302729 |
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