Question: The external flows around a 3D wing are studied at different angles of attack (0-15) while the inlet velocity remains constant at 15 m/s. A

The external flows around a 3D wing are studied at different angles of attack (0-15) while the inlet velocity remains constant at 15 m/s. A schematic view of the wing is shown in the figure below. The aerofoil's chord is 1 m while the wing's span is 2 m

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