THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<
9th Edition
ISBN: 9781266657610
Author: CENGEL
Publisher: MCG CUSTOM
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Textbook Question
Chapter 1.11, Problem 96RP
The average temperature of the atmosphere in the world is approximated as a function of altitude by the relation
Where Tatm is the temperature of the atmosphere in K and z is the altitude in km with z = 0 at sea level. Determine the average temperature of the atmosphere outside an airplane that is cruising at an altitude of 12,000 m.
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Chapter 1 Solutions
THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<
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