Section 3.4 - REVIEW EXERCISE

1. The part of an airplane that produces lift is called a(n) camber decreases airfoil decrease chord .

2. The baseline for designing an airfoil in cross section is determined from the camber decreases airfoil decrease chord .

3. The amount of lift that a wing can produce is determined by the camber decreases airfoil decrease chord .

4. Bernoulli's principle states that as the velocity of a fluid increases, its pressure camber decreases airfoil decrease chord .

5. Lift is produced by the camber decreases airfoil decrease chord in pressure on top of an airfoil as the air passing over the top of the airfoil is     speeded up.

6. Name the parts of the airfoil shown by the arrows.

7. The relative wind is airflow produced by the angle parallel incidence attack aircraft opposite of moving through the air.

8. The relative wind flows in a direction angle parallel incidence attack aircraft opposite of with and angle parallel incidence attack aircraft opposite of to the direction of flight.

9. The angle between the chord of the wing and the longitudinal axis of the aircraft is called the angle parallel incidence attack aircraft opposite of

      angle parallel incidence attack aircraft opposite of angle parallel incidence attack aircraft opposite of .

10. The angle parallel incidence attack aircraft opposite of angle parallel incidence attack aircraft opposite of angle parallel incidence attack aircraft opposite of is the angle between the chord of the wing and the relative wind.