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FAQnewred.gif (906 bytes)           

Section 3.4 - REVIEW EXERCISE

1. The part of an airplane that produces lift is called a(n) .

2. The baseline for designing an airfoil in cross section is determined from the .

3. The amount of lift that a wing can produce is determined by the .

4. Bernoulli's principle states that as the velocity of a fluid increases, its pressure .

5. Lift is produced by the 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.

 

A. 
B. 
C. 
D. 
E. 
F. 

 

7. The relative wind is airflow produced by the moving through the air.

8. The relative wind flows in a direction with and to the direction of flight.

9. The angle between the chord of the wing and the longitudinal axis of the aircraft is called the

      .

10. The is the angle between the chord of the wing and the relative wind.


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