Power calculations for Hovering

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SUMMARY

The discussion focuses on calculating the power required for a hovering helicopter, specifically relating power (P) and thrust (T) at zero velocity. The key takeaway is that while the theoretical minimum power required is zero due to the absence of velocity, practical hovering requires accelerating a mass of air downwards. The larger the propeller diameter, the less power is needed to achieve hover, as it allows for greater air mass acceleration.

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  • Understanding of basic physics principles, particularly force and velocity.
  • Familiarity with helicopter mechanics and aerodynamics.
  • Knowledge of thrust generation and its relationship to weight.
  • Basic calculations involving power and force equations.
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Aerospace engineers, helicopter designers, and hobbyists interested in rotorcraft performance and power calculations for hovering flight.

rosshalz
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Hi,

I have a very basic question. Theoretically,I need to make a load hover (in real terms I'm makin a heli).

I wanted to do the calculations for how much power is needed by the prime mover (engine/motor doesn matter) to hover. i.e to give thrust(T) = weight of (load+Motor).
Can someone please tell me this equation that relates Power(P) and Thrust(T) at zero velocity i.e hovering.

Dont worry about prop diameter/aerodynamic characteristics etc at this moment. I'm just looking for the minimum power of the prime mover(energy source) to give me the ability to hover a certain weight

Thanks!
 
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Unfortunately it's not that simple.

The formula for power is quite simple: Force x Velocity. So the quick answer to your question is that no matter how much your load weighs, the minimum power required is "0", since your velocity is zero. If you think about it, this is precisely true...after all, how much power does it take for the ground to hold up a mountain?

Obviously this isn't the answer you're looking for. A helicopter is not supported by the ground, but by the air. It does this by accelerating a mass of air down, with the reaction keeping it up. The greater this mass of air that is accelerated the closer you can get to the theoretical "0" requirement. Essentially this means that the larger your propeller diameter, the less power you need.
 

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