EBK ESSENTIAL UNIVERSITY PHYSICS, VOLUM
4th Edition
ISBN: 9780135272947
Author: Wolfson
Publisher: VST
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Textbook Question
Chapter 15, Problem 73P
(a) Use the result of Problem 70 to express Earth's atmospheric density as a function of height. (b) Use your result from (a) to find the height below which half of Earth’s atmospheric mass lies (this will require integration).
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What would be the height of the atmosphere if the air density (a) were uniform and (b) decreased linearly to zero with height? Assume
that at sea level the air pressure is 1.00 atm and the air density is 1.25 kg/m³.
(a) Number
Units
(b) Number
i
Units
The pressure on Earth's atmosphere as a function of height y above sea level can be determined by
assuming g to be constant and that the density of air is proportional to the pressure, i.e., px P.
Note that this assumption is not very accurate since temperature and other weather effects can
influence pressure. [Hint: Po = 1.013 × 105 N/m², po = 1.29 kg x m-³]
(1) Start by finding a relation between the pressure Po and the density of air po at 0° at sea level
(y=0) and the pressure P and density p at height y. Using this relation find an expression
for p as a function of P, i.e., p = p(P).
(2) Find the pressure as a function y.
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level?
The basic barometer can be used as an altitudemeasuring device in airplanes. The ground control reports a barometric reading of 753 mmHg while the pilot’s reading is 690 mmHg. Estimate the altitude of the plane from ground level if the average air density is 1.20 kg/m3.
Chapter 15 Solutions
EBK ESSENTIAL UNIVERSITY PHYSICS, VOLUM
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