Power required for helicopter to hover.

In summary, the problem is about finding the power output needed for a second helicopter with half the linear dimensions of the first one to hover. By modeling the helicopter as a sphere and using the principles of volume and area, it is determined that the power output needed is one eighth of the original helicopter. This is due to the decrease in mass and lift of the smaller helicopter. The solution is plausible and power is directly proportional to mass. Rotor diameter does not affect the amount of air moved, but rather the rotation speed.
  • #1
Fruh2theline
3
0

Homework Statement



A helicopter can hover when the output of its engines is P. A second helicopter, an exact copy of the first one, but its linear dimensions are half of those of the original. What power output is needed to enable this second helicopter to fly?


Homework Equations



The teacher describes this problem as being "maximum physics and minimum maths" so I am modeling the helicopter as a sphere for simplicity and working from there.


The Attempt at a Solution



If the helicopter is a sphere then decreasing the radius of the sphere by a half will decrease the volume by an eighth (V is proportional to radius cubed).
If the volume is decreased by an eighth then the mass is decreased by an eighth.

The lift of the blades if proportional to area of the circle they sweep out so decreasing their length by a half will decrease the area of the circle by a quarter (area is proportional to r squared).

So if the weight is decreased by an eighth and the lift from the blades is decreased by a quarter then half of the power of the original helicopter will suffice for this one to hover.

Am I missing anything?
Is this solution plausible?
Thanks for the help.
 
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  • #2
Honestly I think you went further.
The power needed is just one eight of the bigger helicopter.
 
  • #3
It is all about scaling. Power scales with mass (you better try to prove it).

Rotor diameter doesn't matter, as amount of air moved depend not only on rotor diameter, but also on the rotation speed - and it doesn't have to be constant.
 

What is the definition of "Power required for helicopter to hover"?

The power required for a helicopter to hover is the amount of energy needed to keep the helicopter suspended in the air at a constant height and position.

How is the power required for a helicopter to hover calculated?

The power required for a helicopter to hover is calculated by multiplying the weight of the helicopter by its vertical velocity. It takes into account factors such as air density, rotor blade design, and engine efficiency.

What factors affect the power required for a helicopter to hover?

The power required for a helicopter to hover is affected by a variety of factors, including the weight of the helicopter, air density, altitude, temperature, rotor blade design, and engine efficiency.

Why is the power required for a helicopter to hover important?

The power required for a helicopter to hover is important because it helps determine the maximum weight a helicopter can carry, the altitude it can reach, and the amount of fuel it will consume during flight.

How does the power required for a helicopter to hover differ from the power required for forward flight?

The power required for a helicopter to hover is typically higher than the power required for forward flight, as the helicopter must counteract the force of gravity to stay in the air. The power required for forward flight also takes into account the forward motion of the helicopter and the drag from the air.

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