Assume that the density of the atmosphere as a function of altitude h (in kilometers) above sea
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Assume that the density of the atmosphere as a function of altitude h (in kilometers) above sea level is δ(h) = ae−bh 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.
Assume that the density of the atmosphere as a function of altitude h¯y=1Area(D)∬DydA (in kilometers) above sea level is δ(h)=ae−bh kg/km3y, where a=1.225×109f(x,y)=y and b=0.13f(−x,y)=f(x,y). Calculate the total mass of the atmosphere contained in the cone-shaped region √x2+y2≤h≤3D.
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