for Using the information given in Figure 3.3 temperature variation in the atmosphere, create a nice plot that shows how the atmospheric pressure (kPa) varies with increasing elevation up to 15 km above sea-level (where the temperature is 288.15 K (i.e. 15 °C)). In order to match the physical nature of the problem, plot the elevation on the vertical y-axis and atmospheric pressure on the horizontal x-axis (similar to what is done for Figure 3.3).
for Using the information given in Figure 3.3 temperature variation in the atmosphere, create a nice plot that shows how the atmospheric pressure (kPa) varies with increasing elevation up to 15 km above sea-level (where the temperature is 288.15 K (i.e. 15 °C)). In order to match the physical nature of the problem, plot the elevation on the vertical y-axis and atmospheric pressure on the horizontal x-axis (similar to what is done for Figure 3.3).
Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Chapter1: Introduction
Section: Chapter Questions
Problem 1.1P
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Transcribed Image Text:Using the information given in Figure 3.3
for
temperature variation in the atmosphere, create a nice plot that shows how the atmospheric pressure (kPa) varies
with increasing elevation up to 15 km above sea-level (where the temperature is 288.15 K (i.e. 15 °C)). In order to
match the physical nature of the problem, plot the elevation on the vertical y-axis and atmospheric pressure on the
horizontal x-axis (similar to what is done for Figure 3.3).
Transcribed Image Text:Elevation (km)
90
80
70
60
40
30
20
10
1
I
I
I
I
T
-92.5°C
80.0 km
0
-120 -100 -80
-56.5°C
-44.5°C
32.2 km
20.1 km
11.0km
-20.5°C
-60 -40
Temperature (°C)
61.6 km
-20
-2.5°C
52.4 km
47.3 km
15.0°C
Figure 3.3
T = To-mz
where
To = 288.15 K
m = 0.0065 K/m
Troposphere:
201
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