Assume that the density of the atmosphere as a function of altitude h (in kilometers)
Chapter 15, Problem 9(choose chapter or problem)
Assume that the density of the atmosphere as a function of altitude h (in kilometers) above sea level is (h) = aebh kg/km3, where a = 1.225 109 and b = 0.13. Calculate the total mass of the atmosphere contained in the cone-shaped region x2 + y2 h 3.
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