Flight Dynamics - 19AST302

5. Drag caused by the shape and surface roughness of the aircraft.
7. The limits of speed, altitude, and load factor an aircraft can safely operate.
8. A control surface on the wing used to control roll.
9. The main body of the aircraft, holding the crew, passengers, and cargo.
12. Hinged surfaces on the wings used to increase lift during takeoff and landing.
13. Drag caused by the generation of lift.
15. A small vertical surface on the wingtip that reduces drag.
16. A control surface on the tail used to control yaw.
18. The axis running from wingtip to wingtip.
19. The axis running from the top to the bottom of the aircraft.
20. The tail section of an aircraft, including the stabilizers and rudder.

1. The axis running from the nose to the tail of the aircraft.
2. The distance an aircraft can travel horizontally compared to its altitude loss.
3. Surfaces on the wings used to reduce lift and increase drag.
4. The shape of a wing or blade that generates lift.
6. The point where the aircraft's weight is balanced.
10. The ratio of the speed of the aircraft to the speed of sound.
11. A control surface on the tail used to control pitch.
14. The ratio of the lift on an aircraft to its weight.
17. A dimensionless number representing the drag per unit area.