Ideal flow theory will yield a flow pattern past an -rfoil similar to that shown. If the
Chapter 4, Problem 4.91(choose chapter or problem)
Ideal flow theory will yield a flow pattern past an -rfoil similar to that shown. If the approach air velocity V0 is ':> m/s, what is the pressure difference between the bottom and ::1e top of this airfoil at points where the velocities are V1 = 85 m/ s ..:~d V2 = 75 m/s? Assume Pair is uniform at 1.2 kg/m3 .
Unfortunately, we don't have that question answered yet. But you can get it answered in just 5 hours by Logging in or Becoming a subscriber.
Becoming a subscriber
Or look for another answer