walking said:
Homework Statement:: Find the power required to keep a helicopter hovering
Relevant Equations:: P=Fv
View attachment 279993
My thinking was that the power produced by a falling object is P=Fv=(-mg)(-gt)=mg^2t. So it depends on t, ie the "counter power" must also depend on t if it is to balance it, right? But author's solution is a constant. I know I am making a mistake somewhere.
The problem that I see with your thinking is the following:
You are calculating the power of impact of the helicopter against the ground, after free-falling for certain time (no air resistance) or from certain height, which is the same.
Of course, that velocity of impact would depend on the falling time or height.
Nevertheless, your helicopter is not falling; it is instead trying to climb higher and higher in a medium of air, which keeps moving downwards because it is not a very solid substance to cling to.
In reference to your earlier thread, the situation of your helicopter is somehow similar to the situation of a man trying to climb a moving stair in the wrong direction at the same speed the steps are moving down: he is not moving vertically from its position.
The only way the hovering helicopter can counteract the relentless effect of gravity is by inducing a force of equal magnitude and opposite direction to its own weight.
The blades do that by changing the momentum of an endless cylinder of air.
Note that that effect does not depend on the height of the helicopter or the time it would take for the helicopter or the mass of air to reach the ground.
The blades move a certain amount of mass of air by unit of time; therefore, they induce a mass flow rate, which depend on the density of the air, its change in velocity moving down from the blades, and the area covered by the blades disk.
The required power to make all the above happens can be estimated by calculating how much kinetic energy that mass of air gains per unit of time.
Please, see:
https://www.grc.nasa.gov/www/k-12/airplane/thrsteq.html
http://hyperphysics.phy-astr.gsu.edu/hbase/ke.html#c3
Air mass flow rate:
##\dot m=\frac {dm}{dt}=\rho VA_{disk}##
##E_k=\frac 1 2 mV^2##
##Power=\frac 1 2 \dot mV^2=\frac 1 2 \rho A_{disk}V^3=\frac 1 2 \rho \pi r_{blades}^2V^3##