Effect of inlet geometry and Reynolds number on turbine blade leading edge cooling employing jet impingement
An adapter is often required at the entrance of the cooling channel for ease of installation, alignment, leakproof connection, quick removal, or a manufacturing requirement. The present study investigates the effect of the inlet adapter at jet Reynolds numbers (Rej) of 1.047 × 104 and 1.047 × 105 on...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2025-09-01
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| Series: | Case Studies in Thermal Engineering |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2214157X25008354 |
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