Physics for Scientists and Engineers
6th Edition
ISBN: 9781429281843
Author: Tipler
Publisher: MAC HIGHER
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Chapter 13, Problem 85P
To determine
The diameter of the pipeline.
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When a personsnorkels, the lungs are connecteddirectly to the atmosphere throughthe snorkel tube and thus are at atmosphericpressure. In atmospheres,what is the differencebetween this internal air pressureand the water pressure against thebody if the length of the snorkeltube is (a) 20 cm (standard situation) and (b) 4.0 m (probablylethal situation)? In the latter, the pressure difference causesblood vessels on the walls of the lungs to rupture, releasing bloodinto the lungs., an elephant can safelysnorkel through its trunk while swimming with its lungs 4.0 m belowthe water surface because the membrane around its lungscontains connective tissue that holds and protects the blood vessels,preventing rupturing.
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Chapter 13 Solutions
Physics for Scientists and Engineers
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- Scurrilous con artists have been known to represent gold-plated tungsten ingots as pure gold and sell them at prices much below gold value but high above the cost of tungsten. With what accuracy must you be able to measure the mass of such an ingot in and out of water to tell that it is almost pure tungsten rather than pure gold?arrow_forwardThe average human has a density of 945 kg/m3 after in haling and 1 020 kg/m3 after exhaling. (a) Without making any swimming movements, what percentage of the human body would be above the surface in the Dead Sea (a body of water with a density of about 1 230 kg/m3) in each of these cases? (b) Given that bone and muscle are denser than fat, what physical characteristics differentiate sinkers (those who tend to sink in water) from floaters (those who readily float)?arrow_forwardA frequency quoted rule of thumb aircraft design is that wings should produce about 1000 N of lift per square meter of wing. (The fact that a wing has a top and bottom surface does not double its area.) (a) At takeoff, an aircraft travels at 60.0 m/s, so that the air speed relative to the bottom of the wing is 60.0 m/s. Given be sea level density of air as 1.29kg/m3, how fast must it move over be upper surface to create the ideal lift? (b) How fast must air move over the upper surface at a cruising speed of 245 m/s and at an altitude where air density is one-fourth that at sea level? (Note that his not all of be aircraft's lift—some comes from be body of the plane, some from engine thrust, and so on. Furthermore, Bernoulli's principle gives approximate answer because flow over wing creates turbulence.)arrow_forward
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