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
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?
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?