Earth’s atmospheric pressure p is oftenmodeled by assuming that the rate dp/dh at which p changeswith the altitude h above sea level is proportional to p. Supposethat the pressure at sea level is 1013 millibars (about 14.7 poundsper square inch) and that the pressure at an altitude of 20 km is90 millibars. Solve the initial value problemDifferential equation: dp/dh = kp (k a constant)Initial condition: p = p0 when h = 0to express p in terms of h. Determine the values of p0 and kfrom the given altitude-pressure data.
Earth’s atmospheric pressure p is oftenmodeled by assuming that the rate dp/dh at which p changeswith the altitude h above sea level is proportional to p. Supposethat the pressure at sea level is 1013 millibars (about 14.7 poundsper square inch) and that the pressure at an altitude of 20 km is90 millibars. Solve the initial value problemDifferential equation: dp/dh = kp (k a constant)Initial condition: p = p0 when h = 0to express p in terms of h. Determine the values of p0 and kfrom the given altitude-pressure data.
Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
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Question
Earth’s atmospheric pressure p is often
modeled by assuming that the rate dp/dh at which p changes
with the altitude h above sea level is proportional to p. Suppose
that the pressure at sea level is 1013 millibars (about 14.7 pounds
per square inch) and that the pressure at an altitude of 20 km is
90 millibars. Solve the initial value problem
Differential equation: dp/dh = kp (k a constant)
Initial condition: p = p0 when h = 0
to express p in terms of h. Determine the values of p0 and k
from the given altitude-pressure data.
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