Rotation Kinetic Energy of Two Helicopter Blades

In summary, the conversation discusses the calculation of the total moment of inertia and rotational kinetic energy of two blades on a helicopter. The blades have a combined mass of 230 kg and are rotating at an angular speed of 41 rad/s. The moment of inertia can be calculated using the equation for a thin rod, and the kinetic energy can be found using the equation for torque.
  • #1
teddygrams
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A helicopter has two blades (see figure), each of which has a mass of 230 kg and can be approximated as a thin rod of length 6.7 m. The blades are rotating at an angular speed of 41 rad/s. (a) What is the total moment of inertia of the two blades about the axis of rotation? (a) Determine the rotational kinetic energy of the spinning blades.

i know i have to use Torque=I * angular acceleration
but i don't know how all that fits in?
 
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  • #2
i know i have to use Torque=I * angular acceleration

Are you sure about that? The question is asking for the total moment of inertia, which you calculate based on the size and mass of the blades (well you look them up in your book). What's the equation for the moment of inertia of a thin rod?
 
  • #3


I can help you understand the concept of rotational kinetic energy and how it applies to the given scenario.

Firstly, let's define rotational kinetic energy. It is the energy an object possesses due to its rotational motion. In other words, it is the energy required to rotate an object around an axis.

In this case, the two helicopter blades are rotating at an angular speed of 41 rad/s. The moment of inertia of an object is a measure of its resistance to rotational motion and is given by the formula I = mr^2, where m is the mass of the object and r is the distance from the axis of rotation.

Since each blade has a mass of 230 kg and a length of 6.7 m, the moment of inertia of each blade can be calculated as I = (230 kg)(6.7 m)^2 = 10,807.8 kg m^2.

To find the total moment of inertia of the two blades, we simply add the moment of inertia of each blade, giving us a total moment of inertia of 21,615.6 kg m^2.

Now, to determine the rotational kinetic energy of the spinning blades, we use the formula K = 1/2Iω^2, where K is the rotational kinetic energy, I is the moment of inertia, and ω is the angular speed.

Plugging in the values, we get K = 1/2(21,615.6 kg m^2)(41 rad/s)^2 = 45,149,461.2 J.

Therefore, the rotational kinetic energy of the spinning blades is 45,149,461.2 J.

In conclusion, the total moment of inertia of the two helicopter blades is 21,615.6 kg m^2 and the rotational kinetic energy of the spinning blades is 45,149,461.2 J. I hope this helps clarify the concept for you.
 

FAQ: Rotation Kinetic Energy of Two Helicopter Blades

What is rotation kinetic energy?

Rotation kinetic energy is the energy an object possesses due to its rotation around an axis. In the case of helicopter blades, it is the energy that allows the blades to rotate and generate lift.

How is rotation kinetic energy calculated?

The formula for rotation kinetic energy is KE = 1/2 * I * ω^2, where KE is the kinetic energy, I is the moment of inertia, and ω is the angular velocity.

What factors affect the rotation kinetic energy of helicopter blades?

The rotation kinetic energy of helicopter blades is affected by the mass and shape of the blades, the speed at which they rotate, and the distance from the axis of rotation.

How does the rotation kinetic energy of helicopter blades affect flight?

The rotation kinetic energy of helicopter blades is essential for generating lift, which allows the helicopter to take off and stay in the air. Without enough rotation kinetic energy, the helicopter would not be able to lift off the ground.

Can the rotation kinetic energy of helicopter blades be increased?

Yes, the rotation kinetic energy of helicopter blades can be increased by increasing the angular velocity or the mass of the blades. However, this must be done within safe limits to avoid damaging the helicopter or putting it at risk of malfunctioning during flight.

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