## Lift on a Wing

What is the lift (in newtons) due to Bernoulli's principle on a wing of area 76.2 m2 if the air passes over the top and bottom surfaces at speeds of 326 m/s and 282 m/s, respectively?

**1.31×106 N**## Discussion

**NEW**

**Rho**"A LOT OF MONSTER TRUCKS"

Rho of air=1.293 kg/m^3

They give it to you in the next problem, the hurricane

problem. Dunno why they don't give it to you here, but good

luck!

**NEW**

**equation?**

so in the book it says the equation for this is (Pbottom-

Ptop)*A=Ftotal

im confused as to why this is not workng and what does the

above post have to do with it? im clearly missing

soemthing...

**NEW**

*Anonymous 3*

How do I go about solving this problem?