Application of Artificial Neural Network Based Surrogate Models for Parameterized Flow to a Sweptback Wing: An Outlook for Wind Turbine Blades
AIAA SCITECH 2025 Forum
01.01.2025
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Low-speed wind-tunnel investigation of triangular sweptback air inlet in root of 45° sweptback wing
Engineering Index Backfile | 1955
|Prediction of Laminar to Turbulent Flow over a Sweptback Wing
British Library Conference Proceedings | 2012
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