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larisa86 [58]
3 years ago
5

How do you calculate the dynamic lift in an aeroplane?

Engineering
1 answer:
3241004551 [841]3 years ago
8 0

Answer:

the lift equation states that lift L is equal to the lift coefficient CI times the density r times half of the velocity V squared times the wing area A. For given air conditions,shape and inclination of the object, we have to determine a value of CI to determine the lift.

Not really sure but this is all I know

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