Relation between Bernoulli's theorem and aeroplanes

In summary, aeroplanes apply Bernoulli's theorem to calculate the pressure on the top and bottom of the wing, which results in lift. The lift is produced by diverting air downwards and creating pressure differentials, which follows Bernoulli's theorem. However, from the air's frame of reference, work is performed on the air, violating Bernoulli's equation. A demonstration in the London Science Museum shows how the pressure distribution changes on a wing at different angles of attack, but does not show the airflow behind the wing.
  • #1
abhijithmatt
5
0
i heard that aeroplanes are an application of benoulis theorem. Can you please explain it to me.
 
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  • #2
In a way, they are. Provided you take on faith the fact that the air flowing over a wing moves faster over the top than over the bottom, then Bernoulli's theorem, which describes the inverse relationship between pressure and velocity, will allow you to calculate the pressure on the top and the bottom of the wing, and therefore the lift.

Understanding why the air moves faster over the wing is more difficult.
 
  • #3
If you read enough forums you will eventually come across an argument between two groups of people. One camp will be arguing that the lift produced by a wing is due to the application of Benoulis theorem, the other camp will be arguing that lift is produced by the wing accelerating the airflow downwards. It's a false dichotomy.
 
  • #4
A wing produces lift by diverting air downwards. This process involves creation of pressure differentials that coexist with acceleration of air, and the acceleration of air from higher pressure areas to lower pressure areas created by a wing approximately follows Bernoulii's theorem. Bernoulli's basic equation assumes that total energy of the air is not changed, but a wing affects the total energy somewhat, so Bernoulli's equation is an approximation.

The point made by CWatters is that Bernoulli's theorem and downwash theorem both apply to aeroplanes, and that they aren't in conflict.

Using an ideal wing as a frame of reference, it diverts the relative flow downwards without changing the speed, so the total energy remains constant and Bernoulli isn't violated, but from the air's frame of reference, the once still air ends up being accelerated downwards (lift) and somewhat forwards (drag), resulting in a non-zero "exit velocity" (the speed of the affected air when it's pressure first returns to ambient), and in the air's frame of reference work is performed on the air, violating Bernoulli's equation. An efficient wing diverts a large amount of air by a small angle, and from the air's frame of reference, the total energy added to the air is relatively small.
 
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  • #5
Nice explanation.

Just for info.. I recall seeing a demonstration in the London Science Museum some years ago that comprised a section of wing in a simple wind tunnel. It had a set of water filled tubes connected to holes in the top and bottom wing surface that showed the pressure difference between top and bottom surfaces at various points on the chord. You could rotate the wing to change the angle of attack and see how the pressure distribution changed. Nice simple demo of the Bernoulli part of the story but you couldn't see what the airflow behind the wing was doing as there was no smoke system or similar.
 

1. How does Bernoulli's theorem relate to aeroplanes?

Bernoulli's theorem states that as the speed of a fluid (such as air) increases, the pressure exerted by the fluid decreases. In aeroplanes, this principle is utilized to create lift by increasing the speed of air over the wings and decreasing the pressure above the wings, allowing the plane to stay in the air.

2. What is the role of Bernoulli's theorem in the design of aeroplanes?

Bernoulli's theorem is a fundamental principle in the design of aeroplanes. It is used to determine the shape and angle of the wings, as well as the overall aerodynamics of the plane, in order to maximize lift and minimize drag.

3. Can you explain the concept of "lift" in relation to Bernoulli's theorem and aeroplanes?

Lift is the force that allows an aeroplane to stay in the air. According to Bernoulli's theorem, as air moves faster, the pressure decreases. This means that the air moving over the curved upper surface of an aeroplane wing creates a lower pressure than the air moving underneath the flat lower surface. This difference in pressure creates lift and allows the plane to fly.

4. Are there any limitations to Bernoulli's theorem in relation to aeroplanes?

While Bernoulli's theorem is an important principle in aerodynamics, it is not the only factor that affects lift and flight. Other factors such as the angle of attack, air density, and airfoil shape also play a role in the aerodynamics of a plane. Therefore, it is important for aeroplane designers to consider all of these factors in addition to Bernoulli's theorem.

5. How has Bernoulli's theorem influenced the development of aeroplanes?

Bernoulli's theorem has greatly influenced the design and development of aeroplanes. It has allowed for the creation of more efficient and aerodynamic planes, leading to faster and safer air travel. The principles of Bernoulli's theorem are also applied in other areas of aviation, such as helicopter and rocket design.

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