P = 0, x = 0 and a = 1
P=1, x = 0 and a = 0
P = 0, x = 1 and a = 0
X = 0, a + p = 1 Where a = absorptivity, p = reflectivity, X = transmissivity.
D. X = 0, a + p = 1 Where a = absorptivity, p = reflectivity, X = transmissivity.
Kirchhoff's law
Stefan's law
Wines law
Planck's law
Conduction
Convection
Radiation
Conduction and convection
In heat exchanger design as a safety factor
In case of Newtonian fluids
When a liquid exchanges heat with a gas
None of the above
Black bodies
Polished bodies
All coloured bodies
All of the above
Improve heat transfer
Provide support for tubes
Prevent stagnation of shell side fluid
All of these
Grey body
Brilliant white polished body
Red hot body
Black body
S.H/(S.H + L.H)
(S.H + L.H) /S.H
(L.H - S.H)/S.H
S.H/(L.H - S.H)
Watt/mK
Watt/m²K²
Watt/m²K4
Watt/mK²
Black body
Grey body
Opaque body
White body
Higher
Lower
Same
Depends on the area of heat exchanger
k. A. (dT/dx)
k. A. (dx/dT)
k. (dT/dx)
k. (dx/dT)
W/m²K
W/m²
W/mK
W/m
Conduction
Convection
Radiation
Scattering
6
9
27
81
Thermal conductivity to the equivalent thickness of the film of fluid
Temperature drop through the films of fluids to the thickness of film of fluids
Thickness of film of fluid to the thermal conductivity
Thickness of film of fluid to the temperature drop through the films of fluids
Grashoff number and Reynold number
Grashoff number and Prandtl number
Prandtl number and Reynold number
Grashoff number, Prandtl number and Reynold number
m²/hr
m²/hr °C
kcal/m² hr
kcal/m. hr °C
Directly proportional to the surface area of the body
Directly proportional to the temperature difference on the two faces of the body
Dependent upon the material of the body
All of the above
Minimum energy
Maximum energy
Both (A) and (B)
None of these
More than those for liquids
Less than those for liquids
More than those for solids
Dependent on the viscosity
High thickness of insulation
High vapour pressure
Less thermal conductivity insulator
A vapour seal
K cal/kg m² °C
K cal m/hr m² °C
K cal/hr m² °C
K calm/hr °C
Parallel flow type
Counter flow type
Cross flow type
Regenerator type
Quantity of heat flowing in one second through one cm cube of material when opposite faces ^re maintained at a temperature difference of 1°C
Quantity of heat flowing in one second through a slab of the material of area one cm square, thickness 1 cm when its faces differ in temperature by 1°C
Heat conducted in unit time across unit area through unit thickness when a temperature difference of unity is maintained between opposite faces
All of the above
Q = 2πkr1 r2 (T1 - T2)/ (r2 - r1)
Q = 4πkr1 r2 (T1 - T2)/ (r2 - r1)
Q = 6πkr1 r2 (T1 - T2)/ (r2 - r1)
Q = 8πkr1 r2 (T1 - T2)/ (r2 - r1)
k/h₀
2k/h₀
h₀/k
h₀/2k
0
0.5
0.75
1
Is black in colour
Reflects all heat
Transmits all heat radiations
Absorbs heat radiations of all wave lengths falling on it
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
Parallel flow
Counter flow
Cross flow
All of these