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Question: A metal rod of cross-sectional area \(1c{{m}^{2}}\) is being heated at one end. At some instant, the...

A metal rod of cross-sectional area 1cm21c{{m}^{2}} is being heated at one end. At some instant, the temperature gradient is 5Ccm15{}^\circ Cc{{m}^{-1}} at a cross-section AA and is 2.5Ccm12.5{}^\circ Cc{{m}^{-1}} at cross-section BB. The heat capacity of the part ABAB of the rod is 0.4JC10.4J{}^\circ {{C}^{-1}}. Thermal conductivity of the material of the rod is 200Wm1C1200W{{m}^{-1}}{}^\circ {{C}^{-1}}. Neglect any loss of heat to the atmosphere. Calculate the rate at which the temperature is increasing in the part ABAB of the rod.
A) 24Cs124{}^\circ C{{s}^{-1}}
B) 40Cs140{}^\circ C{{s}^{-1}}
C) 12.5Cs112.5{}^\circ C{{s}^{-1}}
D) 48Cs148{}^\circ C{{s}^{-1}}

Explanation

Solution

The given temperature gradients at two instants are used to find the rate of flow of heat at those particular instants. From the expression relating specific heat capacity and rate of heat flow of a conducting material, we can derive the rate of change of temperature within these two instants.

Complete answer:
Let us consider a metal rod of cross-sectional area 1cm21c{{m}^{2}}. One end of the rod is heated. It is obvious that the other end of the rod will get heated in some time. We are supposed to consider two instants of time or two cross- sectional areas AA and BB through which the heat flows. It is given that the temperature gradients on these cross-sectional areas are 5Ccm15{}^\circ Cc{{m}^{-1}} and 2.5Ccm12.5{}^\circ Cc{{m}^{-1}}, respectively. Temperature gradient is a physical quantity which describes the direction of flow of temperature as well as the rate of flow of temperature through a particular location. It is expressed as dTdx\dfrac{dT}{dx}when the flow of temperature is in the xx direction. Let us express the temperature gradient at the cross-section AA as (dTdx)A{{\left( \dfrac{dT}{dx} \right)}_{A}} and the temperature gradient at the cross-section BB as (dTdx)B{{\left( \dfrac{dT}{dx} \right)}_{B}}. Clearly,

(dTdx)A=5Ccm1=500Cm1{{\left( \dfrac{dT}{dx} \right)}_{A}}=5{}^\circ Cc{{m}^{-1}}=500{}^\circ C{{m}^{-1}}
Let this be equation 1.
Also,
(dTdx)B=2.5Ccm1=250Cm1{{\left( \dfrac{dT}{dx} \right)}_{B}}=2.5{}^\circ Cc{{m}^{-1}}=250{}^\circ C{{m}^{-1}}
Let this be equation2.

Now, let us find the rate of flow of heat along ABAB. We know that rate of flow of heat is expressed as
dθdt=KAdTdx\dfrac{d\theta }{dt}=KA\dfrac{dT}{dx}
Where
dθdt\dfrac{d\theta }{dt} is the rate of flow of heat along a section of a heat conducting material
KK is the thermal conductivity of the heat conducting material
AA is the area of the heat conducting material
dTdx\dfrac{dT}{dx} is the temperature gradient at an instant of time, provided the direction of heat flow is in the xx direction.
Let this be equation 1.

We are provided that the thermal conductivity of the metal rod is
K=200Wm1C1K=200W{{m}^{-1}}{}^\circ {{C}^{-1}}
We are also given that the area of cross-section of the metal rod is
a=1cm2=0.0001m2a=1c{{m}^{2}}=0.0001{{m}^{2}}
Let the heat flow along the cross-sectional area AA be (dθdt)A{{\left( \dfrac{d\theta }{dt} \right)}_{A}} and the heat flow along the cross-sectional area BB be (dθdt)B{{\left( \dfrac{d\theta }{dt} \right)}_{B}}. Clearly, from equation 3 and equation 1, we have

(dθdt)A=Ka(dTdx)A=Ka(500)=200×0.0001×500=10Js1{{\left( \dfrac{d\theta }{dt} \right)}_{A}}=Ka{{\left( \dfrac{dT}{dx} \right)}_{A}}=Ka(500)=200\times 0.0001\times 500=10J{{s}^{-1}}
Let this be equation 4.

Also, from equation 3 and equation 2, we have
(dθdt)B=Ka(dTdx)B=Ka(250)=200×0.0001×250=5Js1{{\left( \dfrac{d\theta }{dt} \right)}_{B}}=Ka{{\left( \dfrac{dT}{dx} \right)}_{B}}=Ka(250)=200\times 0.0001\times 250=5J{{s}^{-1}}
Let this be equation 5.

Now, the rate of flow of heat through ABAB is given by
(dθdt)AB=(dθdt)A(dθdt)B=105=5Js1{{\left( \dfrac{d\theta }{dt} \right)}_{AB}}={{\left( \dfrac{d\theta }{dt} \right)}_{A}}-{{\left( \dfrac{d\theta }{dt} \right)}_{B}}=10-5=5J{{s}^{-1}}
Let this be equation 6.

We know the general expression that the change in heat in a conducting material is equal to the product of the heat capacity of the material and the change in temperature.
dθ=CdTd\theta =CdT
where
dθd\theta is the change in heat
CC is the heat capacity of the material
dTdT is the change in temperature
To get the rate of change in heat in the material, let us divide the above equation by dtdt as follows.
dθdt=CdTdt\dfrac{d\theta }{dt}=C\dfrac{dT}{dt}
where
dθdt\dfrac{d\theta }{dt} is the rate of heat flow
CC is the heat capacity of the material
dTdt\dfrac{dT}{dt} is the rate of change of temperature
Let this be equation 7.

Substituting equation 6 in equation 7, we have
(dθdt)AB=C(dTdt)AB{{\left( \dfrac{d\theta }{dt} \right)}_{AB}}=C{{\left( \dfrac{dT}{dt} \right)}_{AB}}
where
(dθdt)AB{{\left( \dfrac{d\theta }{dt} \right)}_{AB}} is the rate of heat flow in the section ABAB of the metal rod
(dTdt)AB{{\left( \dfrac{dT}{dt} \right)}_{AB}} is the rate of temperature change in the section ABAB of the metal rod

Rearranging the above expression,
(dTdt)AB=(dθdt)ABC=50.4=12.5Cs1{{\left( \dfrac{dT}{dt} \right)}_{AB}}=\dfrac{{{\left( \dfrac{d\theta }{dt} \right)}_{AB}}}{C}=\dfrac{5}{0.4}=12.5{}^\circ C{{s}^{-1}}
Therefore, the rate at which temperature is increasing in the part ABAB of the rod is equal to 12.5Cs112.5{}^\circ C{{s}^{-1}}.

So, the correct answer is “Option C”.

Note:
It is important to convert the units of the quantities given in the question to the same unit system. It is always better to convert the values to the International System of Units (SI) for easy calculations. Students need to be thoroughly aware of the SI units of various quantities as well as the related conversions for easy mathematics.