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This produces a greater velocity increase above the wing than below the wing. The greater velocity increases the pressure differential on a cambered airfoil. The greater pressure differential on
the airfoil will increase the magnitude of the aerodynamic force.
SYMMETRIC AIRFOIL
Increasing angle of attack on any airfoil causes the area of the streamtube above the wing to decrease. This produces a greater velocity increase above the wing than below the wing. The greater velocity creates a pressure
differential on a symmetric airfoil. The greater pressure differential on the airfoil will increase the magnitude of the aerodynamic force...
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