What is the lift (in newtons) due to Bernoulli\\'s principle on a wing of area 84 m2 if the air passes over the top and bottom surfaces at speeds of 240 m/s and 150 m/s, respectively?

The area of the wing is $\"\"$ .

The speed of the air passes over the bottom of the wing is $\"\"$ .

The speed of the air passes over the top of the wing is $\"\"$ .

The Bernoullis equation is $\"\"$ .

Since the thickness of wing is small, $\"\"$ is negligible.

$\"\"$ .

The net force on the wing is $\"\"$ .

$\"\"$

The density of air is $\"\"$ .

Substitute $\"\"$ , $\"\"$ and $\"\"$ .

$\"\"$

$\"\"$ .

The net force on the wing is $\"\"$ .