What equation do you use for this?

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SUMMARY

The discussion focuses on calculating the lift force exerted by air on a 4500 kg helicopter that accelerates upward at 2 m/s² using Newton's Second Law. The total lift force must counteract both the gravitational force and provide the necessary force for upward acceleration. The gravitational force is calculated as 4500 kg multiplied by 9.81 m/s², resulting in 44145 N. The total lift force required is therefore 44145 N plus the force needed for acceleration, which is 9000 N, leading to a total lift force of 53145 N.

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a 4500kg helicopter accelerates upward at 2m/s^2 what lift force is exerted by the air on the propellers?
 
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Use Newton's 2nd Law. (Don't forget to include all the forces acting on the helicopter.)
 

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