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Figure shows the cross section of a wall made of three layers. The layer thicknesses are L1,L2=0.700L1,andL3=0.350L1. The thermal conductivities are, k1,k2=0.900k1and k3=0.800k1. The temperatures at the left and right sides of the wall are TH=30.0°°äand TC=−15.0°°ä, respectively. Thermal conduction is steady. (a) What is the temperature difference ΔT2across layer 2 (between the left and right sides of the layer)? If k2were, instead, equal to 1.1k1, (b) would the rate at which energy is conducted through the wall be greater than, less than, or the same as previously, and (c) what would be the value of ΔT2?

Short Answer

Expert verified
  1. Temperature difference ΔT2across layer 2is .15.8°°ä
  2. If,k2=1.1k1then the rate at which energy is conducted through the wall is greater.
  3. Temperature difference localid="1662433196049" ΔT2whenlocalid="1662433188116" k2=1.1k1islocalid="1662433192284" 13.8°°ä.

Step by step solution

01

The given data

  1. ThicknessL2=0.700L1
  2. ThicknessL3=0.350L1
  3. Thermal conductivityk2=0.900k1
  4. Thermal conductivityk3=0.800k1
  5. The temperature oftheleft side of wallTH=30.0°°äor303K
  6. The temperature of the left side of wallTc=−15°°äor258‿é
02

Understanding the concept of Fourier's law of thermal conduction

According to Fourier's Law, the amount of time it takes for heat to go through a material is proportional to the negative gradient of the temperature as well as the cross-sectional area that is perpendicular to the gradient. We will use the equation for the conduction rate through the slab under the assumption that the transfer is a steady-state process, i.e., the temperature everywhere in the slab and the rate of energy transfer do not change with time. In a steady-state process, the conduction rate through the two materials must be constant.

Formula:

The rate at which the sphere emits thermal radiation,Pcond=Qt=kA(TH−TC)L …(¾±)

03

(a) Calculation of the temperature difference

Considering the rate of heat transfer through each layer to be the same, the rate of heat transfer across the entire wallis equal to the rate across layer2(P2). Using equation (i) and cancelling out the common factor of area, we obtain

TH−TCL1k1+L2k2+L3k3=ΔTL2k230°°ä−(−15°°ä)2.21=ΔT27945°°ä2.21=ΔT279ΔT2=15.8°°ä

Hence, the value of temperature difference is15.8°°ä

04

(b) Calculation of the rate of energy of conduction

If k2=1.1k1, then the rate at which energy is conducted through the wall is greater because we are multiplying it by conductivity k2.Hence the conductivity of k2.is going to increase.

05

(c) Calculation of the temperature difference if k2=1.1k1

Repeat the above calculation of part (a) with new value fork2.We get the temperature difference as:

451+711+3580=ΔT2711ΔT2=13.8°°ä

This is less than the result calculated in (a), which shows that the temperature gradient across 1 and 3 is greater than in part (a).The larger temperature gradient leads to large conductive heat currents.

Hence, the required temperature difference is13.8°°ä

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