From sea level to an altitude of 11 km, the standard altitude is based on a linear variation of temperature with altitude, h, where T decreases at a rate of −6.5 K per kilometer (the lapse rate). At sea level, the standard pressure, density, and temperature are 1.01325 × 105 N/m2, 1.2250 kg/m3, and 288.16 K, respectively. Calculate the pressure, density, and temperature at a standard altitude of 5 km.
From sea level to an altitude of 11 km, the standard altitude is based on a linear variation of temperature with altitude, h, where T decreases at a rate of −6.5 K per kilometer (the lapse rate). At sea level, the standard pressure, density, and temperature are 1.01325 × 105 N/m2, 1.2250 kg/m3, and 288.16 K, respectively. Calculate the pressure, density, and temperature at a standard altitude of 5 km.
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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From sea level to an altitude of 11 km, the standard altitude is based on a linear variation of temperature with altitude, h, where T decreases at a rate of −6.5 K per kilometer (the lapse rate). At sea level, the standard pressure, density, and temperature are 1.01325 × 105 N/m2, 1.2250 kg/m3, and 288.16 K, respectively. Calculate the pressure, density, and temperature at a standard altitude of 5 km.
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