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Influence of a Backward-Facing Step on Swept-Wing Boundary-Layer Transition
Experimental measurements were performed on a swept flat-plate model with an airfoil leading edge and imposed chordwise pressure gradient to determine the effects of a backward-facing step on transition in a low-speed stationary crossflow-dominated boundary layer. Detailed hot-wire measurements were...
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| Udgivet i: | AIAA J |
|---|---|
| Main Authors: | , , , |
| Format: | Artigo |
| Sprog: | Inglês |
| Udgivet: |
2019
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| Fag: | |
| Online adgang: | https://ncbi.nlm.nih.gov/pmc/articles/PMC6800700/ https://ncbi.nlm.nih.gov/pubmed/31631890 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.2514/1.J057437 |
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