Heat Transfer: Conduction, Thermal Conductivity, and More

 
Modes of Heat Transfer &
Analysis
 
Dr. J. Badshah
Professor and Head, Dairy Engineering
SANJAY GANDHI INSTITUTE OF DAIRY
TECHNOLOGY
(Bihar Animal Sciences University, Patna)
Email: ejazbadshah@gmail.com
 
Modes of Heat Transfer
 
Conduction
a.
Transfer of heat without appreciable displacement of molecules
forming the substance
b.
In solids conduction by lattice vibration or by transport of free
electrons
c.
In gases, the kinetic energy of the molecules is a function of
temperature and energy is transferred in low temperature region
by collisions
d.
In liquid the molecules are more closely spaced than that of gases
but the mechanism of heat transfer is same as that of gas
e.
Fourier’s law of heat conduction: Q= - KA dt/dx
f.
The decreasing value of temperature gradient (dt/dx) will take care
of –ive sign in above equation.
g.
Area  A is perpendicular to the direction of heat flow, m
2  
 , Q is in
Watt if thermal conductivity K is in W/m. K and dx is the thickness
in m in the direction of heat flow
 
Thermal Conductivity: Essential Features
 
Definition: K = Q/A . dx/dt where Q is heat per unit time
Conduction of heat proportional to K
Heat conduction : In decreasing order of pure metals, alloys
and non metals due to decreasing K values.
K in pure metals varies from  10 to 400 W/m °C, K in Alloys
varies from 12  to 120 W/m °C
K in insulating materials: 0.023 to 2.9 W/m. °C
K in liquid : 0.2 to 0.7 W/m. °C
K in gases and vapours: 0.006 to 0.05 W/m. °C
Dependence of thermal conductivity on Temperature:
K =  K
0
 (1 + 
β
 t), where 
β
 is -1/°C for metals and liquids
(Aluminium, Uranium and water being the exception)
 
Thermal Conductivity: Essential Features
 
In gases the values of K increases with increase in temperature
because  K is proportional to mean molecular path of the
molecules.  But higher molecular weights gases having high density
and low mean molecular path results in lower K values at the
same temperature.
In solids and liquids K depends weakly on pressure but in gases K
is independent of pressure (near atmospheric pressures).
K of damp materials of non metallic solids is considerably higher
and depends on type of gas in the voids.
Wiedmann and Franz Law: The ratio of the thermal (K) and
electrical conductivities (
σ
 ) 
is the same for all metals at the same
temperature. The ratio K/ 
σ
 is proportional to absolute temperature
T  °A for all metals.  
K/ 
σ
  T = C = 2.45 x 10 – 8 W 
/ K
2
 
The materials which are good conductors of electricity  are also
good conductors of heat.
 
Thermal Resistance and Electrical Analogy
 
Electric Circuit Theory has Ohm’s Law: I = V/R
Fourier’s Equation have Q = dt /(dx/KA)
Thermal  Resistance  (dx/KA) is analogous to electrical
resistance R, Q is analogous to electrical current  ‘I’ and
Temperature difference ‘dt’ is analogous to electrical voltage
difference.
Therefore rules for combining electrical resistances in series
and parallel will apply equally to the combination of thermal
resistances.
Calculate the rate of heat transfer per unit area through a
copper plate 45 mm thick, whose one face at 350°C and the
other face at 50°C. Take thermal conductivity of copper as
370 W/m °C.
Q/A  = -K dt/dx =  -370 (50 -350)/0.045 = 2.466 x 10
6 
 W/ sq.
m.
 
Heat Transfer by Convection
 
Newton’ law of cooling: Q = h .A. (t
s
- t
f
)
Factors for film heat transfer coefficient h are:
Thermodynamic and Transport proprties
Nature of flow
Geometry of surface
Prevailing Thermal conditions
Convection Thermal Resistance = 1/ h A
 A hot plate 1 m x 1.5 m is maintained at 300°C. Air at
20°C blows over the plate. If the convective heat transfer
coefficient is 20 W/m
2
 °C. Calculate the rate of heat
transfer.  Solution: Q = 20 x 1.5 x (300-20) = 8400 W
 
 
Heat Transfer by Radiation
 
Laws of Radiation:
 Wein’s Law: wavelength corresponding to the maximum
energy (
λ
m
) is inversely proportional to absolute
temperature of hot body
Kirchhoff’s Law: Emissivity of the body is numerically
equal to its absorptivity for radiant energy from body at the
same temperature.
The Stefan- Boltzmann Law: The law states that the
emissive power of a black body is directly proportional to
fourth power of its absolute temperature i.e. Q 
α
 T
4
Q = F
 σ
   A ( T
1
4
  - T
2
 
4
)
Where, F = A factor depending on geometry and surface
properties, Stefan- Boltzmann constant 
σ
 = 5.67 x 10 
-8
W/m
2
 K
4 
 , T1 and T2 : Temperature in degrees kelvin
 
 
Numericals on modes of heat transfer
 
Solve 5 Numericals on each modes at least.
A carbon steel plate (K = 45 W/m°C) dimension : 600
mm x 900 mm x 25 mm is maintained at 310°C. Air at
15°C blows over the hot plate. If convection heat
transfer coeficient is 22 W/m2 °C and 250 W is lost
from the plate surface by radiation, calculate the inside
plate temperature. In this case Qcond. = Q conv. + Q
radiation
- K  A. dt/dx = h. A ( ts –tf) + 
 F
 σ
   A ( T
1
4
  - T
2
 
4
)
-45x0.54xx (310 – t
i
) /0.025 = 22 x 0.54 (310-15) + 250
Therefore t
i
 = 313.86 °C
 
THANKS TO ALL
THANKS TO ALL
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Explore the fundamentals of heat transfer through conduction and thermal conductivity as explained by Dr. J. Badshah. Learn about the modes of heat transfer, Fourier's law, thermal resistance, and the relationship between thermal and electrical conductivity. Discover the essential features of thermal conductivity in solids, liquids, and gases, along with practical examples and analogies from electrical circuit theory.

  • Heat Transfer
  • Conduction
  • Thermal Conductivity
  • Fouriers Law
  • Thermal Resistance

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  1. Modes of Heat Transfer & Analysis Dr. J. Badshah Professor and Head, Dairy Engineering SANJAY GANDHI INSTITUTE OF DAIRY TECHNOLOGY (Bihar Animal Sciences University, Patna) Email: ejazbadshah@gmail.com

  2. Modes of Heat Transfer Conduction a. Transfer of heat without appreciable displacement of molecules forming the substance b. In solids conduction by lattice vibration or by transport of free electrons c. In gases, the kinetic energy of the molecules is a function of temperature and energy is transferred in low temperature region by collisions d. In liquid the molecules are more closely spaced than that of gases but the mechanism of heat transfer is same as that of gas e. Fourier s law of heat conduction:Q= - KA dt/dx f. The decreasing value of temperature gradient (dt/dx) will take care of ive sign in above equation. g. Area A is perpendicular to the direction of heat flow, m2, Q is in Watt if thermal conductivity K is in W/m. K and dx is the thickness in m in the direction of heat flow

  3. Thermal Conductivity: Essential Features Definition:K = Q/A .dx/dt where Q is heat per unit time Conduction of heat proportional to K Heat conduction : In decreasing order of pure metals, alloys and non metals due to decreasing K values. K in pure metals varies from 10 to 400 W/m C, K in Alloys varies from 12 to 120W/m C K in insulating materials:0.023 to 2.9W/m. C K in liquid :0.2 to 0.7W/m. C K in gases and vapours:0.006 to 0.05W/m. C Dependence of thermal conductivity onTemperature: K = K0(1 + t), where is -1/ C for metals and liquids (Aluminium, Uranium and water being the exception)

  4. Thermal Conductivity: Essential Features In gases the values of K increases with increase in temperature because K is proportional to mean molecular path of the molecules. But higher molecular weights gases having high density and low mean molecular path results in lower K values at the same temperature. In solids and liquids K depends weakly on pressure but in gases K is independent of pressure (near atmospheric pressures). K of damp materials of non metallic solids is considerably higher and depends on type of gas in the voids. Wiedmann and Franz Law: The ratio of the thermal (K) and electrical conductivities ( ) is the same for all metals at the same temperature.The ratio K/ is proportional to absolute temperature T Afor all metals. K/ T = C = 2.45 x 10 8 W / K2 The materials which are good conductors of electricity are also good conductors of heat.

  5. Thermal Resistance and Electrical Analogy Electric CircuitTheory has Ohm s Law:I =V/R Fourier s Equation have Q = dt /(dx/KA) Thermal Resistance resistance R, Q is analogous to electrical current Temperature difference dt is analogous to electrical voltage difference. Therefore rules for combining electrical resistances in series and parallel will apply equally to the combination of thermal resistances. Calculate the rate of heat transfer per unit area through a copper plate 45 mm thick, whose one face at 350 C and the other face at 50 C. Take thermal conductivity of copper as 370W/m C. Q/A = -K dt/dx = -370 (50 -350)/0.045 = 2.466 x 106W/ sq. m. (dx/KA) is analogous to electrical I and

  6. Heat Transfer by Convection Newton law of cooling:Q = h .A.(ts- tf) Factors for film heat transfer coefficient h are: Thermodynamic andTransport proprties Nature of flow Geometry of surface PrevailingThermal conditions ConvectionThermal Resistance = 1/ hA A hot plate 1 m x 1.5 m is maintained at 300 C. Air at 20 C blows over the plate. If the convective heat transfer coefficient is 20 W/m2 C. Calculate the rate of heat transfer. Solution:Q = 20 x 1.5 x (300-20) = 8400W

  7. Heat Transfer by Radiation Laws of Radiation: Wein s Law: wavelength corresponding to the maximum energy ( m) is inversely proportional to absolute temperature of hot body Kirchhoff s Law: Emissivity of the body is numerically equal to its absorptivity for radiant energy from body at the same temperature. The Stefan- Boltzmann Law: The law states that the emissive power of a black body is directly proportional to fourth power of its absolute temperature i.e. Q T4 Q = F A ( T14- T2 Where, F = A factor depending on geometry and surface properties, Stefan- Boltzmann constant = 5.67 x 10 -8 W/m2K4 , T1 and T2 : Temperature in degrees kelvin 4)

  8. Numericals on modes of heat transfer Solve 5 Numericals on each modes at least. A carbon steel plate (K = 45 W/m C) dimension : 600 mm x 900 mm x 25 mm is maintained at 310 C. Air at 15 C blows over the hot plate. If convection heat transfer coeficient is 22 W/m2 C and 250 W is lost from the plate surface by radiation, calculate the inside plate temperature. In this case Qcond. = Q conv. + Q radiation - K A.dt/dx = h.A ( ts tf) + F A( T14- T2 -45x0.54xx (310 ti) /0.025 = 22 x 0.54 (310-15) + 250 Therefore ti= 313.86 C 4)

  9. THANKS TO ALL

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