Displacement of hypersonic boundary layer instability and turbulence through transpiration cooling
Hypersonic boundary-layer transition onset is commonly characterized in wind tunnel experiments by measuring the surface heat transfer rise above the laminar level. Techniques such as infrared thermography and thin film gauges are routinely used in the field. However, when an interfering cooling eff...
| Main Authors: | , , , , , , |
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| Format: | Journal article |
| Language: | English |
| Published: |
AIP Publishing
2024
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