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pro vyhledávání: '"Klewicki, Charles"'
When a chordwise Reynolds number (Re) falls below about $10^5$ the performance of wings and aerodynamic sections become sensitive to viscous phenomena, including boundary layer separation and possible reattachment. Here, detailed measurements of the
Externí odkaz:
http://arxiv.org/abs/2411.05926
We consider the relationship between modal representations obtained from data-driven decomposition methods and Lagrangian Coherent Structures (LCSs). Mode sensitivity is used to describe this analysis as an extension of the model sensitivity framewor
Externí odkaz:
http://arxiv.org/abs/2410.20802