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29 January, 13:55

How do you calculate the dynamic lift in an aeroplane?

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  1. 29 January, 16:22
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    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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