211.
35
1.50 + 0.3
25
F&T p
3) For the Airfoil with the performance characteristics shown here, determine the lift and drag at an angle of attack of 10°. The airfoil has a chord length of 1.4m and a span of 6.8m. Perform the 200km/h at both 200m elevation AND then at 10,000m elevation.
20
Repeat this if the angle of attack is the stall point of 19.60°.
10 15 2025 Angiefk6)
What load could be lifted from the ground at a takeoff speed of 126km/hr when the angle of attack is 15°? The air is 30°C.