Under the same assumptions underlying the model in (1), determine a differential equation governing the growing population P(t) of a country when individuals are allowed to immigrate into the country at a constant rate r > 0. What is the differential equation for the population P(t) of the country when individuals are allowed to emigrate at a constant rate r > 0?
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Textbook Solutions for Advanced Engineering Mathematics
Question
When the mass m of a body moving through a force field is variable, Newton’s second law of motion takes on the form: If the net force acting on a body is not zero, then the net force F is equal to the time rate of change of momentum of the body. That is,
\(F=\frac{d}{d t}(m v)\),
where mv is momentum. Use this formulation of Newton’s second law in Problems 21 and 22.
*Note that when m is constant, this is the same as F = ma.
In Problem 21, suppose \(m(t)=m_{p}+m_{v}+m_{f}(t)\) where \(m_{p}\) is constant mass of the payload, \(m_{pv}\) is the constant mass of the vehicle, and \(m_{f}(t)\) is the variable amount of fuel.
(a) Show that the rate at which the total mass of the rocket changes is the same as the rate at which the mass of the fuel changes.
(b) If the rocket consumes its fuel at a constant rate \(\lambda\), find m(t). Then rewrite the differential equation in Problem 21 in terms of l and the initial total mass \(m(0)=m_{0}\).
(c) Under the assumption in part (b), show that the burnout time \(t_{b}>0\) of the rocket, or the time at which all the fuel is consumed, is \(t_{b}=m_{f}(0) / \lambda\), where \(m_{f}(0)\) is the initial mass of the fuel.
Solution
The first step in solving 1.3 problem number 22 trying to solve the problem we have to refer to the textbook question: When the mass m of a body moving through a force field is variable, Newton’s second law of motion takes on the form: If the net force acting on a body is not zero, then the net force F is equal to the time rate of change of momentum of the body. That is,\(F=\frac{d}{d t}(m v)\), where mv is momentum. Use this formulation of Newton’s second law in Problems 21 and 22.*Note that when m is constant, this is the same as F = ma.In Problem 21, suppose \(m(t)=m_{p}+m_{v}+m_{f}(t)\) where \(m_{p}\) is constant mass of the payload, \(m_{pv}\) is the constant mass of the vehicle, and \(m_{f}(t)\) is the variable amount of fuel.(a) Show that the rate at which the total mass of the rocket changes is the same as the rate at which the mass of the fuel changes.(b) If the rocket consumes its fuel at a constant rate \(\lambda\), find m(t). Then rewrite the differential equation in Problem 21 in terms of l and the initial total mass \(m(0)=m_{0}\).(c) Under the assumption in part (b), show that the burnout time \(t_{b}>0\) of the rocket, or the time at which all the fuel is consumed, is \(t_{b}=m_{f}(0) / \lambda\), where \(m_{f}(0)\) is the initial mass of the fuel.
From the textbook chapter Differential Equations as Mathematical Models you will find a few key concepts needed to solve this.
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