Physics behind the Coanda effect

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In summary, the Coanda effect is the reason an airplane flies. The Coanda effect combines two types of effects: skin friction and void effect. The skin friction effect is related to how a concave surface affects flow in the boundary layer, but that only affects flow in the boundary layer, and that flow is affected depending on if the flow is laminar or turbulent. The void effect is what I call the "receding surface" effect, and after the peak of a cambered surface flows through a volume of air, the surface recedes from the air, and the air has to fill in what would otherwise be a void. This explains how the air gets pushed down and causes the airplane to rise.
  • #1
aerofreak
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Hi guys,

I was interested in the Coanda effect (what makes an airplane fly) and i was wondering if anyone, in somple terms, could explain the physics behind this to me.

Thanks in advance!
 
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  • #2
Coanda effect for aircraft combines two types of effects. One is related to skin friction and a concave surface, but that only affects flow in the boundary layer, and that flow is affected depending on if the flow is laminar or turbulent. The other effect is what I call void effect, or more appropriately void abhorence effect. After the peak of a cambered surface flows through a volume of air, the surface recedes from the air, and the air has to fill in what would otherwise be a void. Wiki's article on wings also explains this aspect of lift:

In that case a low pressure region is generated on the upper surface of the wing which draws the air above the wing downwards towards what would otherwise be a void after the wing had passed.

http://en.wikipedia.org/wiki/Wing#Science_of_wings

Not covered in the Wiki articleis how the air fills in that "void". Most of the time the path of least "resistance" (accceleration) is for the air to accelerate mostly downwards and somewhat forwards, so you get lift with minimal drag. The other flow pattern that occurs when the angle of attack is excessive, is for the air to form one or more vortices, sort of a giant and turbulent boundary layer, with a much lower amount of lift.

Void effect is clearly understood when streamlining high speed land vehicles. Long tapered tails are used to gradually introduce a void into the air, which allows the air to accelerate at a relatively slow inwards rate, as opposed to accelerating forwards at a much faster rate which occurs if the aft surface is essentially a vertical wall, like a bus.
 
  • #3
Hey rcgldr, thanks for the info. What you explained makes sense.
Would you however also state that the Coanda effect is the reason that airplanes fly? The conservation of momentum, will cause the air to flow of the trailing edge of the wing, forcing air down, which in its turn, forces the plane up (this also explain how experimental flying saucers can fly). Or would you say that the effects you outlined above have more to do with Bernoulli´s theorum?
 
  • #4
aerofreak said:
Would you however also state that the Coanda effect is the reason that airplanes fly?
It's the reason pressure is lowered above the wing. Simple deflection is the reason pressure is increased below the wing. Both effect contribute to lift, although for a conventional wing, most of the lift (more than 1/2) is due to lowering pressure above a wing.

The conservation of momentum, will cause the air to flow of the trailing edge of the wing, forcing air down, which in its turn, forces the plane up (this also explain how experimental flying saucers can fly). Or would you say that the effects you outlined above have more to do with Bernoulli´s theorum?
Downwards acceleration and flow of air starts to occur above a wing, not behind it. It's a dynamic situation where air flows downwoards towards the wing, which move forwards before that flow reaches the surface of a wing. Bernoulli explains how air reacts to pressure differentials within the air (ignoring issues like turbulence), but doesn't explain how those pressure differentials are created by interaction between a wing and the air. This website has some good but simple explanations:

http://www.avweb.com/news/airman/183261-1.html
 
  • #5


The Coanda effect is a phenomenon in fluid dynamics where a fluid (such as air) tends to follow the curvature of a nearby surface rather than continuing in a straight path. This effect is responsible for the lift generated by airplane wings and is an important concept in aerodynamics.

The physics behind the Coanda effect can be explained by the principles of Bernoulli's equation and Newton's third law of motion. According to Bernoulli's equation, as the velocity of a fluid increases, its pressure decreases. This means that as air flows over the curved surface of an airplane wing, the air on the top of the wing has a higher velocity and lower pressure compared to the air on the bottom of the wing. This creates a pressure difference, with lower pressure on top and higher pressure on the bottom, which results in lift.

Newton's third law of motion states that for every action, there is an equal and opposite reaction. In the case of an airplane wing, the air flowing over the curved surface exerts a downward force on the wing, while the wing exerts an equal and opposite force upwards. This upward force is what we call lift and is what allows airplanes to fly.

In summary, the Coanda effect is a result of the combination of Bernoulli's equation and Newton's third law of motion. The curved shape of an airplane wing causes air to flow over the top surface at a higher velocity, creating a pressure difference and resulting in lift. This is the fundamental physics behind the Coanda effect and its role in the flight of airplanes.
 

1. What is the Coanda effect?

The Coanda effect is a phenomenon in fluid dynamics where a fluid stream follows a curved surface instead of continuing in a straight line. This is due to the difference in pressure and velocity in the fluid flow caused by the curved surface.

2. How does the Coanda effect work?

The Coanda effect works due to the Bernoulli's principle, which states that an increase in the speed of a fluid results in a decrease in pressure. When a fluid flows over a curved surface, the air particles near the surface are slowed down, causing a decrease in pressure. The higher pressure on the other side of the curved surface then pushes the fluid stream towards the surface, causing it to follow the curved path.

3. What are some real-life applications of the Coanda effect?

The Coanda effect has various applications in engineering and aerodynamics. It is used in the design of aircraft wings, where the curved shape of the wing helps in generating lift. It is also used in the design of air conditioning systems, exhaust systems, and even in household products like hair dryers.

4. What factors affect the Coanda effect?

The Coanda effect is influenced by several factors, including the shape and curvature of the surface, the speed of the fluid, and the viscosity of the fluid. A more curved surface and higher fluid velocity increase the Coanda effect, while higher viscosity reduces it.

5. Can the Coanda effect be controlled?

Yes, the Coanda effect can be controlled by changing the shape and curvature of the surface, as well as adjusting the fluid velocity. This is essential in engineering applications where the Coanda effect needs to be manipulated for optimal performance.

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