The average temperature of the atmosphere in the world is approximated as a function of altitude by the relation Tatm=288.15- 6.5z where Tam 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 33.000 ft. Convert the calculated temperature in degree Rankine.

The average temperature of the atmosphere in the world is approximated as a function of altitude by the relation Tatm=288.15- 6.5z where Tam 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 33.000 ft. Convert the calculated temperature in degree Rankine.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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