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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

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

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Heat and Mass Transfer
Depending on the radiating properties, body will be transparent when(Where a = absorptivity, p = reflectivity, x = transmissivity)

P=1, x = 0, and a = 0
X = 0, a + p = 1
P = 0, x = 0 and a = 1
P = 0, x= 1, and a = 0

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Heat and Mass Transfer
Thermal diffusivity of a substance is given by (where h = Thermal diffusivity, ρ = Density of substance, S = Specific heat, and k = Thermal conductivity)

h = kρ/S
h = ρS/k
h = S/ρk
h = k/ ρS

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Heat and Mass Transfer
The most commonly used method for the design of duct size is the

Static regains method
Dual or double method
Equal friction method
Velocity reduction method

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Heat and Mass Transfer
Stefan Boltzmann law is applicable for heat transfer by

Radiation
Conduction and radiation combined
Conduction
Convection

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Heat and Mass Transfer
The rate of energy emission from unit surface area through unit solid angle, along a normal to the surface, is known as

Reflectivity
Transmissivity
Emissivity
Intensity of radiation

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