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Heat and Mass Transfer

Heat and Mass Transfer
The ratio of the thickness of thermal boundary layer to the thickness of hydrodynamic boundary layer is equal to (Prandtl number) n, where n is equal to

1
=-1/3
=-2/3
-1

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Heat and Mass Transfer
Thermal conductivity of air with rise in temperature

Decreases
Increases
Remain constant
May increase or decrease depending on temperature

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Heat and Mass Transfer
The rate of heat flow through a body is Q = [kA (T₁ - T₂)]/x. The term x/kA is known as

Thermal resistance
Thermal coefficient
Thermal conductivity
None of these

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Heat and Mass Transfer
Heat is closely related with

Temperature
Liquids
Entropy
Energy

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Heat and Mass Transfer
In a heat exchanger with one fluid evaporating or condensing, the surface area required is least in

Counter flow
Parallel flow
Cross flow
All of these

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Heat and Mass Transfer
The ratio of the emissive power and absorptive power of all bodies is the same and is equal to the emissive power of a perfectly black body. This statement is known as

Planck's law
Kirchhoff's law
Wien's law
Stefan's law

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