Why does a helicopter lift off the ground?

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Discussion Overview

The discussion revolves around the mechanisms of lift generation in helicopters, focusing on the interaction between rotor blades and air. Participants explore concepts related to air pressure, forces, and the terminology used to describe these interactions, with an emphasis on the nuances of "pulling" and "pushing" air.

Discussion Character

  • Debate/contested
  • Technical explanation
  • Conceptual clarification

Main Points Raised

  • Some participants propose that lift is generated by accelerating air, with ambiguity surrounding the term "pushing" as it relates to force application.
  • Others argue that a helicopter both pulls and pushes air, though the definition of "pull" is contested.
  • A participant suggests that the rotor creates a low-pressure zone above it, allowing air to fill the void, which is seen as a relevant mechanism for lift.
  • There is a discussion about the Coanda Effect and airfoil pressure profiles, with some noting that the top surface of an airfoil typically produces most of the lift.
  • Questions arise regarding how pressure differences are determined and whether they are measured relative to atmospheric pressure or freestream conditions.
  • Some participants challenge the relevance of pressure differences in the context of action/reaction forces between the wing and air, emphasizing local pressure differences.
  • There is a debate about the practicality of measuring pressures and how they relate to the net force on objects like doors or wings.
  • Participants discuss the implications of reference pressures in calculations and their real-world significance.

Areas of Agreement / Disagreement

Participants express multiple competing views on the mechanisms of lift generation, the definitions of forces involved, and the relevance of pressure measurements. The discussion remains unresolved, with no consensus reached on key points.

Contextual Notes

Limitations include the ambiguity in terminology, the dependence on definitions of forces, and unresolved questions about pressure measurement methods and their implications for understanding lift.

  • #31
russ_watters said:
Blowing across? I don't think that situation changes the static pressure on the door.
You can change the total pressure on the side of the door with the flow. The static pressure remains on the other side. This is all assuming the door is closed (as with the spacecraft hatch example).

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.
Okay.
 
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  • #32
sophiecentaur said:
How does that make sense?
Well, it doesn't to me. Seems arbitrary.
 
  • #33
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.
The two things have nothing to do with each other. No matter what you use as a reference, you can observe and quantify which side changes more -- it isn't affected by the choice of reference. That's what "arbitrary" means!

Let's say you have a parcel of still air. Call the pressure 14.7 psi. Call it zero. Call it -47. It doesn't matter: when a wing flies through it, the pressure of the air above the wing goes down and the pressure of the air below the wing goes up, both can be measured or calculated separately and the change in the upper surface is usually greater than the change for the lower surface.

Arbitrarily, let's plug in some numbers:

Let's call our reference pressure -47 psi.

Above the wing, the pressure is measured at -49 and below the wing, the pressure is measured at -46. So the pressure above the wing went down by 2psi and the pressure below it went up by 1psi. So the upper surface contributed 2/3 of the lift.

No matter what you pick for the reference, the answer remains the same.

Something else to consider here is that the wing itself is probably not air tight and certainly doesn't contain a vacuum. The completely separate aerodynamic forces on the top and bottom surfaces need to be considered separately when designing the structure of the wing. IE: even though you might think there is a pressure of 14psi pushing down on the top surface of the wing, the rivets holding the top surface on the wing are under tension, not compression.
 
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  • #34
sophiecentaur said:
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.)
What I think AT isn't getting about which side is "responsible" is that it isn't the difference between the two that you need to look at to see which is "responsible", but the change in each that you need to look at. The change in pressure above the wing is usually larger than the change in pressure below the wing.

For a door to a house after you turn an exhaust fan on in the house, the pressure inside changed and the pressure outside didn't. So it is what is happening inside that causes the force on the door.
 
  • #35
This thread had morphed into the same old thread about lift. People seem to assume that the pressure above and below the wing are uniform and static. They are beguiled by the simple wind tunnel idea. What ultimately keeps the plane up there is (has to be) the net downward acceleration of air. The details of air flow around the wing and well beyond it must have an effect.
It is far more complicated than the simple ideas that are being aired here.
 
  • #36
russ_watters said:
What I think AT isn't getting about which side is "responsible" is that it isn't the difference between the two that you need to look at to see which is "responsible", but the change in each that you need to look at.
I get what you mean. I just think that your definition of "responsible" is arbitrary. Those discussions about "causes" of lift are bad enough. But this goes a step further and tries to quantify the contribution of opposing forces to the net force on an object.
 
  • #37
Thank You very much dear friends for an informative discussion!
Through your valuable arguments,my commonsense ideas improved to indepth ones and I got motivation to study and think more.
 

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