Assume that the density of the atmosphere as a function of altitude h (in kilometers) above sea level is ?(h) = ae−bh kg/km3, where a = 1.225 × 109 and b = 0.21. Calculate the total mass M of the atmosphere contained in the cone-shaped region sqrt x2 + y2 ≤ h ≤ 3. (If you enter your answer in scientific notation, round the decimal value to three decimal places. Use equivalent
Assume that the density of the atmosphere as a function of altitude h (in kilometers) above sea level is ?(h) = ae−bh kg/km3, where a = 1.225 × 109 and b = 0.21. Calculate the total mass M of the atmosphere contained in the cone-shaped region sqrt x2 + y2 ≤ h ≤ 3. (If you enter your answer in scientific notation, round the decimal value to three decimal places. Use equivalent
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Assume that the density of the atmosphere as a function of altitude h (in kilometers) above sea level is
?(h) = ae−bh kg/km3,
where
a = 1.225 × 109
and
b = 0.21.
Calculate the total mass M of the atmosphere contained in the cone-shaped region
sqrt | x2 + y2 |
(If you enter your answer in scientific notation, round the decimal value to three decimal places. Use equivalent rounding if you do not enter your answer in scientific notation.)
M= _kg
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