Calculating Lift Force of Helicopter Propellers

In summary, the lift force acting upon the propellers is -41,202 N. The net force is calculated by subtracting the force of gravity from the force of lift, which results in a negative value due to the downward direction of gravity.
  • #1
chemguy990
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0

Homework Statement


A 5400 kg helicopter accelerates upward at 2.17 m/s2. The acceleration due to gravity is 9.8 m/s2. What life force is exerted by the air on the propellers? Answer in N.


Homework Equations


Fnet=ma



The Attempt at a Solution



I am making the acceleration positive (2.17m/s2) and the gravitational acceleration negative (-9.8 m/s2) since the helicopter is traveling upwards.

F(lift) - F(gravity) = ma
F(lift) - (5400kgx(-9.8m/s2)) = (5400kg)(2.17 m/s2)
F(lift) = 11718-52920 N
F(lift) = -41202 N

Shouldnt the lift force acting upon the propellers by positive?
 
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  • #2
Sure!
Net force means the SUM of all forces, positive and negative.
Thus, you have a minus too much here:

F(lift)+F(grav)=ma
F(Lift)=ma-F(grav), remember that F(grav) is here a negative quantity.
 
  • #3


Yes, the lift force should be positive since it is acting in the same direction as the acceleration of the helicopter. Therefore, the correct solution should be:

F(lift) = ma + F(gravity)
F(lift) = (5400 kg)(2.17 m/s^2) + (5400 kg)(9.8 m/s^2)
F(lift) = 11718 N + 52920 N
F(lift) = 64638 N

The lift force exerted by the air on the propellers is 64638 N. This is the force that is responsible for lifting the helicopter off the ground.
 

Related to Calculating Lift Force of Helicopter Propellers

What is lift force?

Lift force is the upward force generated by a helicopter propeller that allows it to stay in the air. It is the result of the difference in air pressure between the top and bottom of the propeller blades.

How is lift force calculated for helicopter propellers?

Lift force is calculated using the equation: Lift Force = 0.5 x Air Density x Velocity^2 x Blade Area x Lift Coefficient. The lift coefficient takes into account the shape and angle of the propeller blades, while the air density and velocity are variables that can change depending on the environment and conditions.

What factors can affect the lift force of helicopter propellers?

The lift force of helicopter propellers can be affected by factors such as air density, propeller speed, propeller blade angle, and the design and shape of the propeller blades. Environmental factors like altitude, temperature, and air pressure can also impact lift force.

Why is calculating lift force important for helicopter propellers?

Calculating lift force is important for helicopter propellers because it helps determine the amount of thrust needed for the helicopter to take off, hover, and maneuver in the air. It also allows for the design and optimization of propellers for different types of helicopters and environments.

Are there any limitations to calculating lift force for helicopter propellers?

Yes, there are limitations to calculating lift force for helicopter propellers. The calculations may not account for all variables that can affect lift force, and there may be variations in air density and velocity that can impact the accuracy of the calculations. Additionally, other factors such as vibrations and air turbulence can also affect the lift force of helicopter propellers.

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