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## LIFT 

## MAGNUS EFFECT 

The explanation of lift can best be explained by looking at a cylinder rotating in an airstream. The local velocity near the cylinder is composed of the airstream velocity and the cylinder’s rotational velocity, which decreases with distance from the cylinder. On a cylinder, which is rotating in such a way that the top surface area is rotating in the same direction as the airflow, the local velocity at the surface is high on top and low on the bottom. 

As exists where the airstream line that impinges on the sur- face splits; some air goes over and some under. Another stagnation point streams rejoin and resume at identical velocities. We 

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now have upwash ahead of the rotating cylinder and downwash at the rear. 

The difference in surface velocity accounts for a differ- ence in pressure, with the pressure being lower on the top than the bottom. This low pressure area produces an upward force known as the “Magnus Effect.” This mechanically induced circulation illustrates the rela- tionship between circulation and lift. 

An airfoil with a positive angle of attack develops air circulation as its sharp trailing edge forces the rear stagnation point to be aft of the trailing edge, while the front stagnation point is below the leading edge. [Figure 2-8] 

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## BERNOULLI’S PRINCIPLE 

Air flowing over the top surface accelerates. The airfoil is now subjected to Bernoulli’ effect.” As air velocity increases through the constricted portion of a venturi tube, the pressure decreases. 

