P = 0, x = 0 and a = 1
P= 1, T = 0 and a = 0
P = 0, x = 1 and a = 0
X = 0, a + p = 0 Where a = absorptivity, p = reflectivity, X = transmissivity.
A. P = 0, x = 0 and a = 1
It is impossible to transfer heat from low temperature source to t high temperature source
Heat transfer by radiation requires no medium
All bodies above absolute zero emit radiation
Heat transfer in most of the cases takes place by combination of conduction, convection and radiation
Domestic refrigerators
Water coolers
Room air conditioners
All of these
Kirchoffs law
Stefan's law
Wien' law
Planck's law
Temperature
Wave length
Physical nature
All of the above
Face area
Time
Thickness
Temperature difference
Absolute temperature
T²
T⁵
T
20°C
40°C
60°C
66.7°C
Nature of the body
Temperature of the body
Type of surface of the body
All of these
Less than those for gases
Less than those for liquids
More than those for liquids and gases
More or less same as for liquids and gases
Absolute temperature (T)
I²
F
T
h₁ + h₂ + h₃
(h₁.h₂.h₃)1/3
1/h₁ + 1/h₂ + 1/h₃
None of these
Change vapour into liquid
Change liquid into vapour
Increase the temperature of a liquid of vapour
Convert water into steam and superheat it
At all temperatures
At one particular temperature
When system is under thermal equilibrium
At critical temperature
Fourier equation
Stefan-Boltzmann equation
Newton Reichmann equation
Joseph-Stefan equation
Steam
Solid ice
Melting ice
Water
Solids
Liquids
Gases
None of these
Its temperature
Nature of the body
Kind and extent of its surface
All of the above
Absorptive power
Emissive power
Absorptivity
Emissivity
Q = [2πlk (T₁ - T₂)]/2.3 log (r₂/r₁)
Q = 2.3 log (r₂/r₁)/[2πlk (T₁ - T₂)]
Q = [2π (T₁ - T₂)]/2.3 lk log (r₂/r₁)
Q = = 2πlk/2.3 (T₁ - T₂) log (r₂/r₁)
The heat transfer in liquid and gases takes place according to convection.
The amount of heat flow through a body is dependent upon the material of the body.
The thermal conductivity of solid metals increases with rise in temperature
Logarithmic mean temperature difference is not equal to the arithmetic mean temperature difference.
Density
Coefficient of viscosity
Gravitational force
All of these
tm = (Δt1 - Δt2)/ loge (Δt1/Δt2)
tm = loge (Δt1/Δt2)/ (Δt1 - Δt2)
tm = tm = (Δt1 - Δt2) loge (Δt1/Δt2)
tm = loge (Δt1 - Δt2)/ Δt1/Δt2
Irregular surfaces
Nonuniform temperature surfaces
One dimensional cases only
Two dimensional cases only
Kirchhoff's law
Stefan's law
Wines law
Planck's law
P = 0, x = 0 and a = 1
P=1, x = 0, and a = 0
P = 0, T= 1, and a = 0
X = 0, a + p = 1
Absorptive power
Emissive power
Emissivity
None of these
Both the fluids at inlet (of heat exchanger where hot fluid enters) are in their coldest state
Both the fluids at inlet are in their hottest state
Both the fluids at exit are in their hottest state
One fluid is in hottest state and other in coldest state at inlet
Equal to
Directly proportional to
Inversely proportional to
None of these
Cold body to hot body
Hot body to cold body
Smaller body to larger body
Larger body to smaller body
Increases
Decreases
Remain constant
May increase or decrease depending on temperature