Helicopter - Variable Air Density

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Discussion Overview

The discussion revolves around the relationship between air density and the energy required to operate helicopter blades, particularly during descent. Participants explore theoretical implications, practical considerations, and related concepts such as ground effect.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant questions whether the energy required to turn helicopter blades is directly proportional to air density, suggesting that as air density increases during descent, the energy might not necessarily increase proportionally.
  • Another participant argues that while the helicopter needs to maintain lift, it may require less volume of air as it descends, indicating that drag may increase but not in direct proportion to air density.
  • A different viewpoint proposes that energy requirements might actually decrease as the helicopter approaches the ground, emphasizing that lift is related to the momentum change of air rather than energy change.
  • One participant highlights the complexity of the situation, noting that maintaining constant rotation speed in denser air could lead to increased lifting power, complicating the relationship between energy and air density.
  • Another participant introduces the concept of ground effect, questioning its influence on helicopters compared to fixed-wing aircraft and suggesting historical challenges in demonstrating helicopter functionality.

Areas of Agreement / Disagreement

Participants express differing views on the relationship between air density and energy requirements for helicopter blades, with no consensus reached. The discussion includes multiple competing perspectives and uncertainties regarding the effects of air density and ground effect.

Contextual Notes

Participants acknowledge the abstract nature of the model being discussed and the complexities involved in real-world helicopter dynamics, including turbulence and the effects of ground proximity.

jaketodd
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This is not homework.

If you descend toward the ground in a helicopter, the density of the air is going to increase. I'm curious: Is the amount of energy required to turn the blades directly proportional to the density of the air? For instance: If the air density doubles, does the energy to turn the helicopter blades double (with a constant rate of blade rotation through both scenarios)?

Thanks,

Jake
 
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Not exactly. Because the chopper needs the same amount of lift at all times accept when accelerating up or down, as it decends, it needs to move less volume of air. Drag will probably increase a little, but not in direct proportion to the air density.
 
It's possible the amount of energy would decreases as you approach the ground, rather than increases. The reason is that the lift force is related to the change or momentum of the air, not the change of energy, and in general it is a more efficient use of energy to create thrust by moving a large mass or air slowly, rather than a small mass of air fast.

But I don't claim to be an expert of helicopter rotors, so I'm only saying that is "possible", not that it's a "fact".
 
First of all, your question is obviously a very abstract model. If any half-way realistic approximation tried to maintain the same rotation speed in denser air, it would simply shoot away with increased lifting power.

Couple that with the fact that the airflow around the blades isn't laminar in nature, it is or can be very much turbulent, thank you. This means that if you find an answer to your question which can fit in this space, please inform Sykorsky and you are set for life :-)

With those caveats, the answer to you question has to be yes - simply because the blades need to displace a larger mass of air which will take away kinetic energy directly proprtional to the mass of the displaced air. However, this is so far removed from reality, I hesitate to even call it an answer.
 
I'm not a round-wing weirdie, but I would love to get my mitts on one sometime before I croak (preferably not immediately before I croak...) While I'm familiar with autorotation and other principles, there is one thing that I've never seen addressed. Does "ground effect" influence whirlybirds in anything similar to the way it does fixed-wing critters?
 
Danger said:
Does "ground effect" influence whirlybirds in anything similar to the way it does fixed-wing critters?

Absolutely. As I remember from the history of the issue, one of the major challenges for tne early attempts was to demostrate that what they got is a true chopper as opposed to hovercraft which depends on the condensed/compressed air cushion to stay afloat.
 
Cool. Thanks, Grizz.
 

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