1. Blood flowing through an artery reaches a place where the artery is narrowed. The speed of the blood in the narrow section __________.
a. increases
b. decreases
c. remains the same
d. is unpredictable
Answer: _____
2. The radius of a pipe carrying water increases by a factor of two. As a result, the speed of the water in the pipe ___________________.
a. increases by a factor of two
b. decreases by a factor of two
c. increases by a factor of four
d. decreases by a factor of four
Answer: _____
3. Water flows through a horizontal tapered pipe. At the wide end its speed is 4.0 m/s and at the narrow end it is 5.0 m/s. The pressure in the wide pipe is 2.5 x 105 Pa. What is the pressure in the narrow pipe?
a. 2.5 x 102 Pa
b. 3.4 x 103 Pa
c. 4.5 x 103 Pa
d. 2.3 x 105 Pa
e. 8.0 x 105 Pa
Answer: _____
4. What is the unit for rgh in Bernoulli’s equation?
a. kg/m3
b. N/m2
c. N/m
d. N m
Answer: _____
5. The speed of the air across the top of an airplane wing is 241 m/s when the speed of the air below the wing is 226 m/s. What is the lifting force if the area of the wing is 24.0 m2?
a. 1.92 x 105 N
b. 4.52 x 103 N
c. 8.40 x 104 N
d. 1.09 x 105 N
Answer: _____
6. A diameter of a stream of water from a faucet decreases as the distance from the faucet’s spout increases. This is a result of __________________.
a. Archimedes’ Principle
b. Pascal’s Principle
c. Bernoulli’s Law and the Equation of Continuity
d. Pascal’s Principle and Bernoulli’s Law
e. Pascal’s Principle and the Equation of Continuity
Answer: _____
7. Bernoulli’s Equation is based upon _____________________.
a. conservation of energy
b. conservation of momentum
c. the second law of motion
d. the third law of motion
Answer: _____
8. The equation of continuity is based on the conservation of ______________.
a. momentum
b. energy
c. mass
d. angular momentum
e. none of the above
Answer: _____
9. Water at a pressure of 3.5 x 105 Pa is flowing at 5.0 m/s in a pipe which narrows to 1/3 its former area. What is the pressure and velocity of the water in the narrow section?
a. 2.5 x 105 Pa, 15 m/s
b. 3.0 x 105 Pa, 10 m/s
c. 3.0 x 105 Pa, 15 m/s
d. 4.5 x 105 Pa, 1.5 m/s
e. 5.5 x 105 Pa, 1.5 m/s
Answer: _____
10. Where is the air pressure the greatest around the airplane wings?
a. In diagonal currents
b. Above
c. Below
d. Opposite the flaps
Answer: _____