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...
| Հիմնական հեղինակներ: | , , , , , , |
|---|---|
| Ձևաչափ: | Journal article |
| Լեզու: | English |
| Հրապարակվել է: |
AIP Publishing
2024
|