Find the lift on an airfoil using Figure 4.12 and Table 2.1 given the following information:

AOA = 12°

Wing area, S = 110 ft2 TAS = 130 kts.

Pressure altitude = 8000 ft Temperature – Standard Day

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Level stall airspeed at gross weight is 38 kts. Stall speed: 41 kts. 30 Stall speed: 45 kts. Stall speed: 53 kts. 45 60 TAS 40 mph Turn radius 185 ft Turn radius 107 ft Turn radius 062 ft TAS 60 mph Turn radius ft Turn radius 0 ft Turn radius 139 ft TAS 80 mph Turn radius740 ft Turn radius 8 ft. Turn radius 24 ft