The change of pressure, Op/an, across a curved streamline can be described by the expression =...

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The change of pressure, Op/an, across a curved streamline can be described by the expression = V2 R where p is fluid density, V is fluid velocity and R is streamline curvature. Using this expression for the pressure gradient, explain how wings generate lift. The change of pressure, Op/an, across a curved streamline can be described by the expression = V2 R where p is fluid density, V is fluid velocity and R is streamline curvature. Using this expression for the pressure gradient, explain how wings generate lift.