Transonic buffet on infinite swept wings arises from coexisting 2D shock oscillations and 3D separation instabilities, with mean separation at the shock required for the 3D cells to dominate.
Vc is related to the Strouhal numberStas Vc =λ z ·f=λ z St·U ∞,2D c ,(9) based on the airfoil chord ofc= 1
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Scale-resolving simulations and data-driven modal analysis of turbulent transonic buffet cells on infinite swept wings
Transonic buffet on infinite swept wings arises from coexisting 2D shock oscillations and 3D separation instabilities, with mean separation at the shock required for the 3D cells to dominate.