Across
- 2. must be increased to maintain the original airspeed and altitude while turning
- 4. of Attack is the angle between chord and relative airflow
- 6. they are designed to increase the lift of the wing at lower speeds
- 7. Located in the leading edge of the wing & is a fixed duct
- 8. is the all up weight (AUW) of the aircraft divided by the wing area
- 9. It occurs when the angle of attack becomes so great that the energy in the air flowing over the wing can no longer pull air down to the surface
Down
- 1. increases with increase in lift
- 2. The Lift on the wings during the _______ is greater than the Lift which the wings have to supply during straight flight
- 3. it is a movable slot
- 5. _______ increases with increasing the angle of attack
- 7. it is the minimum speed the aircraft can fly without stalling