Coanda Effect: Helicopter Rotor Downwash & Lift

  • Thread starter P K Pillai
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In summary, the downwash from a helicopter rotor, if passed over a suitable surface below the rotor could produce a Coanda Effect. Will this influence lift? Beyond the ground effect? What are your thoughts?Thanks.
  • #1
P K Pillai
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The downwash from a helicopter rotor, if passed over a suitable surface below the rotor could produce a Coanda Effect. Will this influence lift?
 
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  • #2
P K Pillai said:
The downwash from a helicopter rotor, if passed over a suitable surface below the rotor could produce a Coanda Effect. Will this influence lift?

Beyond the ground effect? What are your thoughts?
 
  • #3
Thanks.I have insufficient knowledge of the aeronautical sciences to comment on ground effects or on the shape & size of the surface/s that will generate a Coanda.Just a thought experiment.
( formerly VU2BXD ).
 
  • #4
The downwash is already pointing down. Using the Coandă effect to redirect the flow is only going to reduce the lift, though you could get some thrust out of it in return. This is already what the blades are designed to do, however, without any additional surface, so including a surface like that really gains you nothing and, due to the second law of thermodynamics, actually loses you some.
 
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  • #5
The lift generated by a helicopter is created by the blade airfoil section, not by the down stream draft.
Any down draft drag on the fuselage is wasteful, as it will drag the helicopter body downwards.

A helicopter blade has very little, if any, twist along it's length, so only a short section of the blade is working at optimum efficiency. That enables a helicopter to get lift from both sides of the rotor when flying horizontally. But it also means that the maximum down draft is at a different distance away from the fuselage on each side and is airspeed dependent.
It would be quite hard to predict where that down draft would be under operating conditions.
 
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  • #6
Baluncore said:
The lift generated by a helicopter is created by the blade airfoil section, not by the down stream draft.

Those aren't really independent - the airfoil produces a downdraft (it's how it works), and that is why lift is generated. Boneh3ad is correct - any redirection of this downwash is going to reduce the lift generated.
 
  • #7
cjl said:
Those aren't really independent
Nothing is truly independent. The downwash is a reaction to the lift generated by the airfoil.

cjl said:
Boneh3ad is correct - any redirection of this downwash is going to reduce the lift generated.
Yes, Boneh3ad is correct, I never doubted it. Increasing lift by interfering with the downwash is the same as trying to lift yourself by your own boot laces, or a snake eating it's own tail.

It becomes obvious when you consider the downwash as an historical artefact of the blade's lift, rather than implementing a postmodernist analysis/confusion of everything being inseparably connected.
 
  • #8
Baluncore said:
Nothing is truly independent. The downwash is a reaction to the lift generated by the airfoil.

It's really more of a chicken and egg kind of thing. One doesn't really "cause" the other (lift and downwash, that is). Rather, you simply can't have one without the other. They are simply the opposite ends of Newton's laws.
 
  • #9
Baluncore said:
Increasing lift by interfering with the downwash is the same as trying to lift yourself by your own boot laces, or a snake eating it's own tail.
That is not always true, for example, the increase in lift when hovering in ground effect.

But I agree the OP's idea is very unlikely to work.

Baluncore said:
Nothing is truly independent.
Baluncore said:
... rather than implementing a postmodernist analysis/confusion of everything being inseparably connected.
You seem to be contradicting yourself there :confused:
 
  • #10
I agree that lift will be dependent on air density and that “ground effect” can therefore provide increased support to an aircraft when the downdraft flow downstream is impeded by something more fixed than clear air. Ground effect can save even more energy when an aircraft lands on the ground and stops it's engines.

AlephZero said:
You seem to be contradicting yourself there
Science is the contradiction.
Science employs a reductionist approach to analyse a complex universe.
If things were truly independent there would be more than one universe.
Only by modelling simplistic closed hypothetical universes, is science possible.

P.S. The egg came first, then the chicken.
The chicken is the best way eggs have of reproducing themselves.
 
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What is the Coanda Effect?

The Coanda Effect is a phenomenon in fluid dynamics where a fluid (such as air) tends to follow a curved surface instead of moving in a straight line.

How does the Coanda Effect relate to helicopter rotor downwash?

In a helicopter, the rotor blades create a downward flow of air known as downwash. This downwash can be redirected and intensified by using the Coanda Effect, which increases the lift force and helps the helicopter stay in the air.

What factors affect the strength of the Coanda Effect on a helicopter rotor?

The strength of the Coanda Effect on a helicopter rotor is affected by several factors, including the shape and curvature of the rotor blades, the speed and angle of the airflow, and the density and viscosity of the fluid (air).

How does the Coanda Effect help increase lift on a helicopter?

By utilizing the Coanda Effect, helicopter designers can create rotor blades with specific shapes and angles that redirect the downwash and increase the lift force. This allows the helicopter to generate more lift and stay airborne.

Are there any other applications of the Coanda Effect besides helicopter rotors?

Yes, the Coanda Effect has been used in various engineering and design applications, such as in aircraft wings, exhaust systems, and fluid pumps. It has also been studied for potential applications in renewable energy and propulsion systems.

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