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What is the equation of lift?
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What is the equation of lift?

User BiGXERO
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  • lift coefficient Cl times the density r times half of the velocity V squared times the wing area A. L = Cl * A * .5 * r * V^2.

  • For given air conditions, shape, and inclination of the object, we have to determine a value for Cl to determine the lift.

hope it helps!

User Ietu
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