A wing section of L=1m and width 20m is being tested at STP conditions. The speed of the air passing over the bottom surface is 290m/s while the speed distribution over the top surface can be approximated by v(x)= (vox)/L; [0,L] vo=540m/s Based on Bernoulli's principle, determine the lift (the net force) acting on the wing. (The air flows in the x-direction.)