Name: なぜ翼の上ではトップフローが速くなるのですか？ (Why is the top flow faster over an Airfoil ?)
Uploaded: 2021-01-14T06:49:56.000Z
Duration: 4 min 12 s
Description: VoiceTubeの動画で発音を聞きながら英語表現を覚えよう！学べる英語：

様態の副詞

when you closely examine the science behind airfoils.

Why does the air above the airfoil flow much faster than the air below?

The answer is right there in the pressure gradient.

we will first describe how the pressure gradient is developed.

we learned that the flow gets curved as shown to the kiwanda effect.

You can explain the pressure distribution

by keeping in mind that in a curved flow pressure is higher at the outside.

There are three main flow curvatures in this flow.

The biggest is at the top of the airfoil.

Far away from the airfoil the pressure is atmospheric

pressure will decrease as we move toward the airfoil.

The second curvature is at the bottom of the airfoil near the tail,

so here if we move toward the airfoil, the pressure should increase.

The last flow curvature is also at the bottom of the airfoil

this curvature, however, is curved slightly upward.

This means that the pressure should decrease in this region

there will be a very small drop in pressure.

We know that far away from the upstream and downstream

a high-pressure region is generated as the flow directly hits this portion

so we can easily construct the pressure distribution as shown

The CFD results could form exactly two are logical conclusions.

we can neglect this very small drop in pressure.

the pressure decreases almost to the midpoint before it increases

at the bottom the pressure keeps on increasing

and consider two fluid particles starting at the same speed

The top particle is surrounded by a decreasing pressure condition

while the bottom particle sits in an increasing pressure condition.

For the top particle pressure on the right side is less than at the left side

so there will be a net force in the same direction of the velocity

However, the reverse is true for the bottom particle

here the net forces against velocity direction

In short, in a decreasing pressure filled the fluid particle will accelerate

and in an increasing pressure filled the fluid particle will decelerate.

This is exactly what happens in an airfoil also

the bottom particle will keep on decelerating

the top particle will accelerate up to the midpoint.

This means that the speed of the top particle

The bottom particle also experiences of pressure decreasing scenario,

However, it is almost after the trailing edge and it happened suddenly

such a sudden drop in pressure will not considerably increase the particle speed.

the pressure distribution makes the particles flow at different speeds

the different speeds of the particles are not what make the pressure distribution

there is no logical explanation for what causes this speed difference?

These two arguments are not too different ways of looking at the same thing.

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なぜ翼の上ではトップフローが速くなるのですか？ (Why is the top flow faster over an Airfoil ?)

scenario

phenomenon

slightly

force