Abstract
The leading-edge boundary-layer (LEBL) flow is found in the front part of swept airplane wings where the flow is subject to strong acceleration.
Cite
CITATION STYLE
APA
John, M. O., Obrist, D., & Kleiser, L. (2018). Secondary instability and subcritical transition in the leading-edge boundary layer. ERCOFTAC Series, 24, 333–339. https://doi.org/10.1007/978-3-319-63212-4_42
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