An aircraft has the CL curve shown in Figure 4.12. The following data applies: Weight = 20

An aircraft has the CL–α curve shown in Figure 4.12. The following data applies:

Weight = 20 000 lb Wing area, S = 340 ft²

Density altitude = 10 000 ft TAS = 242.4 kts.

Find the aircraft’s AOA for steady flight:_____

Transcribed Image Text:

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