This is wrong.
First of all lets clarify some ideas:
1. Lift is a force, and in fluid dynamics forces are the results of pressure differential.
2. The concept that the bigger the velocity, the lower the pressure is based on Bernoulli's equation (conservation of energy), but this can be applied only on the same streamline (see post on lines in FD).
3. There is no law or experiment that states that the particles that split at the leading edge must combine at the trailing edge at the same time; actually there is evidence that in order to create lift, the particles on the upper surface reach the trailing edge before those on the lower surface.
The correct explanation is the following.
The shape of the aerofoil creates pressure gradients; for a curved streamline, the pressure will be higher on the convex side. This pressure differential accounts for the force; from the force and pressure the velocity is derived.
From this the conclusion is that aerofoil profile is the most important for the lift; a straight profile can't create lift.
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