..60 GO Figure Figure 18-46 shows the cross section of a wall made of three layers. The layer thicknesses are L₁, L2=0.700L₁, and L3=0.350L₁. The thermal conductivities are k₁, k₂ = 0.900k₁, and k3= 0.800k₁. The temperatures at the left side and right side of the wall are TH = 30.0°C and Tc = -15.0°C, respectively. Ther- mal conduction is steady. (a) What is the temperature difference AT₂ across layer 2 (between the left and right sides of the layer)? If k₂ were, instead, equal to 1.1k₁, (b) would the rate at which energy is con- ducted through the wall be greater than, less than, or the same as pre- viously, and (c) what would be the value of AT₂?

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..60 GO Figure
Figure
18-46 shows the
cross section of a wall made of three
layers. The layer thicknesses are
L₁, L2=0.700L₁, and L3=0.350L₁.
The thermal conductivities are k₁,
k₂ = 0.900k₁, and k3= 0.800k₁. The
temperatures at the left side and right
side of the wall are TH = 30.0°C and
Tc = -15.0°C, respectively. Ther-
mal conduction is steady. (a) What
is the temperature difference AT₂
across layer 2 (between the left and
right sides of the layer)? If k₂ were,
instead, equal to 1.1k₁, (b) would
the rate at which energy is con-
ducted through the wall be greater
than, less than, or the same as pre-
viously, and (c) what would be the
value of AT₂?
TH
k₁
k₂ kg
Tc
L₁
L2 L3
Figure 18-46 Problem 60.
Air
Ice
Water
Transcribed Image Text:..60 GO Figure Figure 18-46 shows the cross section of a wall made of three layers. The layer thicknesses are L₁, L2=0.700L₁, and L3=0.350L₁. The thermal conductivities are k₁, k₂ = 0.900k₁, and k3= 0.800k₁. The temperatures at the left side and right side of the wall are TH = 30.0°C and Tc = -15.0°C, respectively. Ther- mal conduction is steady. (a) What is the temperature difference AT₂ across layer 2 (between the left and right sides of the layer)? If k₂ were, instead, equal to 1.1k₁, (b) would the rate at which energy is con- ducted through the wall be greater than, less than, or the same as pre- viously, and (c) what would be the value of AT₂? TH k₁ k₂ kg Tc L₁ L2 L3 Figure 18-46 Problem 60. Air Ice Water
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