# Bernoullis theorem states a the pressure of a fluid

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8. Bernoulli’s theorem states
9. Generally, as altitude increases, temperature will
10. The acute angle formed by the chord line of a wing and the relative wind is known as the
11. Interference drag is reduced by
4 12. The distance between the upper and lower surfaces on an airfoil is called the
13. Lift acts
14. Laminar flow is most likely to occur on an aircraft wing where the skin surface is
15. The center of pressure is also referred to as the
16. The chord of a wing is measured from
17. The net result of lift and drag vectors is
18. Lift varies
19. The curvature of the wing surface is called
20. A stall is the direct result of
21. Supersonic airflow passing through a constriction would be characterized by
22. The speed of sound is
23. As the speed of sound increases
24. The speed of the aircraft in relation to the speed of sound is called
25. The critical Mach number of any airplane is reached
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