Why does a helicopter lift off the ground?

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SUMMARY

The discussion centers on the mechanics of helicopter lift, emphasizing that lift is generated by the acceleration of air rather than merely pushing air downwards. Participants clarify that a helicopter both pulls and pushes air through its rotor blades, creating a low-pressure zone above the rotor that contributes to lift. The conversation highlights the importance of understanding aerodynamic forces, particularly the pressure differences above and below the rotor blades, which are crucial for lift generation. The role of local pressures and the Coanda Effect are also discussed as key concepts in understanding how helicopters achieve lift.

PREREQUISITES
  • Aerodynamics principles
  • Understanding of the Coanda Effect
  • Knowledge of pressure differentials in fluid dynamics
  • Familiarity with airfoil design and lift generation
NEXT STEPS
  • Study the Coanda Effect in detail and its applications in aerodynamics
  • Learn about pressure differential measurement techniques in fluid dynamics
  • Explore the principles of airfoil design and how it affects lift
  • Research the role of local atmospheric pressure in aerodynamic performance
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Aerospace engineers, physics students, and anyone interested in the mechanics of flight and helicopter aerodynamics will benefit from this discussion.

A.T.
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russ_watters said:
For air propelled devices, accelerating the air through it, not that air pushing on the air below it, is what causes the lift.
Agreed. The misunderstanding comes from the ambiguity of the word "pushing". I interpreted it as "applying a force", so a helicopter is pushing the air that it accelerates.

[mod note: split from here: https://www.physicsforums.com/showthread.php?t=762789 ]
 
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A.T. said:
Agreed. The misunderstanding comes from the ambiguity of the word "pushing". I interpreted it as "applying a force", so a helicopter is pushing the air that it accelerates.
I think we're on the same page now except that if we want to go that far we should split that hair as well: the helicopter BOTH pulls and pushes the air that goes through its rotor.
 
russ_watters said:
the helicopter BOTH pulls and pushes the air
You are using ambiguous terms again. What does "pull" mean exctly? Exerting an attractive force? The rotor blade cannot do that. There are only repulsive forces in collisions of air molecules and blade.
 
It gravitationally pulls the air to it. :-pMaybe "sucks" would be a better word. Its sucks the air above it by creating a low pressure zone which allows the air above to fill the void.
 
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A.T. said:
You are using ambiguous terms again. What does "pull" mean exctly? Exerting an attractive force? The rotor blade cannot do that. There are only repulsive forces in collisions of air molecules and blade.
There are two ways to see a "pull":

1. The Coanda Effect.
2. Airfoil pressure profiles are typically normalized to atmospheric pressure, so the pressure on the top surface is indeed typically shown as negative.

The common view that an airfoil pushes the air down tends to cause people to miss the fact that the top surface usually produces most of the lift.
 
ModusPwnd said:
Its sucks the air above it by creating a low pressure zone which allows the air above to fill the void.
True but not directly relevant to action/reaction between helicopter and air. The total force by the air on the helicopter is fully accounted for by the repulsive forces in the collisions between helicopter and air.
 
russ_watters said:
the top surface usually produces most of the lift.
How is that determined? When there is a pressure difference between two sides of a door, can you tell which side of the door produces the net force on the door?
 
From his post it looks like it is determined relative to atmospheric pressure.
 
ModusPwnd said:
From his post it looks like it is determined relative to atmospheric pressure.
You mean the difference in pressure to somewhere far away from the wing, is greater above the wing than below the wing? Well, that again is not directly relevant to action/reaction transfer between wing and air, which is local. The aerodynamic force is fully accounted for by the difference in local pressures at different sides of the wing.
 
  • #10
A.T. said:
You mean the difference in pressure to somewhere far away from the wing, is greater above the wing than below the wing? Well, that again is not directly relevant to action/reaction transfer between wing and air, which is local. The aerodynamic force is fully accounted for by the difference in local pressures at different sides of the wing.
You seem to be suggesting that the pressures above and below are measured relative to each other. Not only is it not done that way, I don't see a practical way that it could be. No: the pressures are measured relative to freestream.

In any case, this tangent has outlived its usefulness and we should get on it. My point in continuing it was mostly just to point out that it is a tangent and not part of the OP's question.
 
  • #11
russ_watters said:
You seem to be suggesting that the pressures above and below are measured relative to each other.
I didn't say anything about pressure measurements or their practicality. I say that the total aerodynamic force on the wing is fully accounted for by the difference in local pressures at different sides of the wing.
 
  • #12
ModusPwnd said:
From his post it looks like it is determined relative to atmospheric pressure.

If a pressure difference is involved, it doesn't matter what the reference pressure is (as long as they both use the same). To analyse the motion, it is easiest to use the Earth frame.
 
  • #13
russ_watters said:
You seem to be suggesting that the pressures above and below are measured relative to each other. Not only is it not done that way, I don't see a practical way that it could be. No: the pressures are measured relative to freestream.

In any case, this tangent has outlived its usefulness and we should get on it. My point in continuing it was mostly just to point out that it is a tangent and not part of the OP's question.

Is "freestream" in a wind tunnel or measured with a probe on the flying craft?
 
  • #14
A.T. said:
How is that determined? When there is a pressure difference between two sides of a door, can you tell which side of the door produces the net force on the door?

Actually there are some devices than can do that. But unless it's likely to rip the door apart, does it really matter?
 
  • #15
A.T. said:
When there is a pressure difference between two sides of a door, can you tell which side of the door produces the net force on the door?
olivermsun said:
Actually there are some devices than can do that.
How?
 
  • #16
A.T. said:
I didn't say anything about pressure measurements or their practicality. I say that the total aerodynamic force on the wing is fully accounted for by the difference in local pressures at different sides of the wing.
Difference in pressure between what and what? You understand that whether it is measured or calculated, a differential pressure is between two points, right?
 
  • #17
russ_watters said:
Difference in pressure between what and what?
Between the two sides of the wing.

The local absolute pressure on the wing surface represents the local density of momentum transfer by the collisions of air molecules with the wing, involving only repulsive forces. The surface integral of this absolute pressure on the wing gives you the total aerodynamic force on the wing. No pulling involved here.
 
  • #18
A.T. said:
How?
A "pressure sensor." Although, in this case you could argue that the whole door is a (differential) pressure sensor. :biggrin:

Although now that I think about it, I don't see how you could say the force on one side of the door or the other is what "produces" the net force. Isn't it the sum of forces = the differential pressure what produces the "net" force?
 
  • #19
A.T. said:
How?
Typically, by identifying what caused the pressure difference; wind? A fan?
 
  • #20
sophiecentaur said:
Is "freestream" in a wind tunnel or measured with a probe on the flying craft?
You didn't describe two different methods, but just two different situations that are equivalent: you can reference free stream static pressure with the same probe whether it is in a wind tunnel or outside.
 
  • #21
olivermsun said:
Although now that I think about it, I don't see how you could say the force on one side of the door or the other is what "produces" the net force. Isn't it the sum of forces = the differential pressure what produces the "net" force?
Exactly. That's why I don't understand this:

russ_watters said:
the top surface usually produces most of the lift.
 
  • #22
A.T. said:
Exactly. That's why I don't understand this:
Because in reality, there is a reference pressure. You can subtract it out in the math to create a different reference*, but that doesn't actually make it go away in the real world.

*in some cases you might, in others you wouldn't.
 
  • #23
olivermsun said:
Although now that I think about it, I don't see how you could say the force on one side of the door or the other is what "produces" the net force. Isn't it the sum of forces = the differential pressure what produces the "net" force?
Because something had to add force to one side or take it away from the other. A fan, for example.

Let's simplify: you measure the differential pressure across the escape hatch of a spaceship in orbit. Can you say which side the force is being applied to?
 
  • #24
russ_watters said:
Because in reality, there is a reference pressure.
The aero dynamic force depends only on the difference in pressures between the sides of the wing, not on how these pressures compare to some reference pressure far away from the wing.
 
  • #25
russ_watters said:
Because something had to add force to one side or take it away from the other. A fan, for example.
So is a fan blowing across one side of the door "pulling" the door or is the static pressure on the other side of the door "pushing" the door? Doesn't it depend on which phenomenon you choose to focus upon?

Let's simplify: you measure the differential pressure across the escape hatch of a spaceship in orbit. Can you say which side the force is being applied to?
I'd have to say air pressure is being applied mostly to the inside surface, since the ambient pressure on the outside is probably pretty small.
 
  • #26
russ_watters said:
Let's simplify: you measure the differential pressure across the escape hatch of a spaceship in orbit.
So, what is the "reference pressure" here, and why?
 
  • #27
A.T. said:
The aero dynamic force depends only on the difference in pressures between the sides of the wing, not on how these pressures compare to some reference pressure far away from the wing.
Ignoring it doesn't make it go away. You asked how you can tell which side is most responsible for the lift and the answer is what it is. Not sure what else can be said.

So, what is the "reference pressure" here, and why?
Space is chosen as the reference because it is convenient/useful.
 
  • #28
olivermsun said:
So is a fan blowing across one side of the door "pulling" the door or is the static pressure on the other side of the door "pushing" the door? Doesn't it depend on which phenomenon you choose to focus upon?
Blowing across? I don't think that situation changes the static pressure on the door.

I was thinking more along the lines of a fan blowing into or out of the room though another opening, either positively or negatively pressurizing it with respect to the other side.
I'd have to say air pressure is being applied mostly to the inside surface, since the ambient pressure on the outside is probably pretty small.
Agreed.
 
  • #29
russ_watters said:
Space is chosen as the reference because it is convenient/useful.
If the choice of reference pressure is so arbitrary, then so is the claim about which side is most responsible for the net force.
 
  • #30
A.T. said:
If the choice of reference pressure is so arbitrary, then so is the claim about which side is most responsible for the net force.

How does that make sense? It is the difference that counts and that involves both sides; you can't have a 'difference' between one side. They are both "responsible" (if you want to apportion blame lol.)
 

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