Optimistic Calculation of Upward Thrust from Helicopter Blades

What is the upward thrust generated by the spinning blades of a helicopter?

Given a 15007 kg helicopter accelerating upward at 2.3417 m/s^2, how can we calculate the upward thrust from the blades?

Calculation of Upward Thrust

By using the equation Thrust = mass x acceleration, we can determine the upward thrust generated by the spinning blades of the helicopter.

Helicopters rely on the upward thrust created by their spinning blades to lift off the ground. In this scenario, with a helicopter weighing 15007 kg and accelerating upward at 2.3417 m/s^2, we can calculate the upward thrust as follows:

Thrust = mass x acceleration

Plugging in the given values:

Thrust = 15007 kg x 2.3417 m/s^2 = 35193.1 N

Rounding to the nearest whole number, the upward thrust from the blades is approximately 35193 N. This calculation shows the impressive force generated by the spinning blades to lift the helicopter into the sky.