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Short notes for Heat transfer 
Fo u r ie r ’s Law of Heat Conduction 
 
• Q = Heat transfer in given direction. 
• A = Cross-sectional area perpendicular to heat flow direction. 
• dT = Temperature difference between two ends of a block of thickness dx 
• dx = Thickness of solid body 
•  = Temperature gradient in direction of heat flow. 
General Heat Conduction Equation 
• Carterisan Coordinates (side parallel to x, y and z-directions) 
 
       q g = Internal heat generation per unit volume per unit time 
       t = Temperature at left face of differential control volume 
       k x, k y, k z = Thermal conductivities of the material in x, y and z-directions respectively 
       c = Specific heat of the material 
       ? = Density of the material 
        a = Thermal diffusivity  
        dt = Instantaneous time. 
 
o For homogeneous and isotropic material 
 
o For steady state condition (P oi ss on ’s equation) 
 
o For steady state and absence of internal heat generation (Laplace equation) 
 
o For unsteady heat flow with no internal heat generation 
Page 2


Short notes for Heat transfer 
Fo u r ie r ’s Law of Heat Conduction 
 
• Q = Heat transfer in given direction. 
• A = Cross-sectional area perpendicular to heat flow direction. 
• dT = Temperature difference between two ends of a block of thickness dx 
• dx = Thickness of solid body 
•  = Temperature gradient in direction of heat flow. 
General Heat Conduction Equation 
• Carterisan Coordinates (side parallel to x, y and z-directions) 
 
       q g = Internal heat generation per unit volume per unit time 
       t = Temperature at left face of differential control volume 
       k x, k y, k z = Thermal conductivities of the material in x, y and z-directions respectively 
       c = Specific heat of the material 
       ? = Density of the material 
        a = Thermal diffusivity  
        dt = Instantaneous time. 
 
o For homogeneous and isotropic material 
 
o For steady state condition (P oi ss on ’s equation) 
 
o For steady state and absence of internal heat generation (Laplace equation) 
 
o For unsteady heat flow with no internal heat generation 
 
• Cylindrical Coordinates 
o For homogeneous and isotropic material, 
 
o For steady state unidirectional heat flow in radial direction with no internal heat 
generation, 
 
 
• Spherical Coordinates 
o For homogeneous and isotropic material 
 
o For steady state uni-direction heat flow in radial direction with no internal heat 
generation, 
 
• Thermal resistance of hollow cylinders  
 
 
  
• Thermal Resistance of a Hollow Sphere 
 
• Heat Transfer through a Composite Cylinder 
 
Page 3


Short notes for Heat transfer 
Fo u r ie r ’s Law of Heat Conduction 
 
• Q = Heat transfer in given direction. 
• A = Cross-sectional area perpendicular to heat flow direction. 
• dT = Temperature difference between two ends of a block of thickness dx 
• dx = Thickness of solid body 
•  = Temperature gradient in direction of heat flow. 
General Heat Conduction Equation 
• Carterisan Coordinates (side parallel to x, y and z-directions) 
 
       q g = Internal heat generation per unit volume per unit time 
       t = Temperature at left face of differential control volume 
       k x, k y, k z = Thermal conductivities of the material in x, y and z-directions respectively 
       c = Specific heat of the material 
       ? = Density of the material 
        a = Thermal diffusivity  
        dt = Instantaneous time. 
 
o For homogeneous and isotropic material 
 
o For steady state condition (P oi ss on ’s equation) 
 
o For steady state and absence of internal heat generation (Laplace equation) 
 
o For unsteady heat flow with no internal heat generation 
 
• Cylindrical Coordinates 
o For homogeneous and isotropic material, 
 
o For steady state unidirectional heat flow in radial direction with no internal heat 
generation, 
 
 
• Spherical Coordinates 
o For homogeneous and isotropic material 
 
o For steady state uni-direction heat flow in radial direction with no internal heat 
generation, 
 
• Thermal resistance of hollow cylinders  
 
 
  
• Thermal Resistance of a Hollow Sphere 
 
• Heat Transfer through a Composite Cylinder 
 
 
• Heat Transfer through a Composite Sphere 
 
 
• Critical Thickness of Insulation:  
o In case of cylinder, 
 
where, k 0 = Thermal conductivity, and h = Heat transfer coefficient 
o The drop in temperature across the wall and the air film will be proportional to their 
resistances, = hL/k. 
  
 
• Steady Flow of Heat along a Rod Circular fin 
?=pd 
 
Page 4


Short notes for Heat transfer 
Fo u r ie r ’s Law of Heat Conduction 
 
• Q = Heat transfer in given direction. 
• A = Cross-sectional area perpendicular to heat flow direction. 
• dT = Temperature difference between two ends of a block of thickness dx 
• dx = Thickness of solid body 
•  = Temperature gradient in direction of heat flow. 
General Heat Conduction Equation 
• Carterisan Coordinates (side parallel to x, y and z-directions) 
 
       q g = Internal heat generation per unit volume per unit time 
       t = Temperature at left face of differential control volume 
       k x, k y, k z = Thermal conductivities of the material in x, y and z-directions respectively 
       c = Specific heat of the material 
       ? = Density of the material 
        a = Thermal diffusivity  
        dt = Instantaneous time. 
 
o For homogeneous and isotropic material 
 
o For steady state condition (P oi ss on ’s equation) 
 
o For steady state and absence of internal heat generation (Laplace equation) 
 
o For unsteady heat flow with no internal heat generation 
 
• Cylindrical Coordinates 
o For homogeneous and isotropic material, 
 
o For steady state unidirectional heat flow in radial direction with no internal heat 
generation, 
 
 
• Spherical Coordinates 
o For homogeneous and isotropic material 
 
o For steady state uni-direction heat flow in radial direction with no internal heat 
generation, 
 
• Thermal resistance of hollow cylinders  
 
 
  
• Thermal Resistance of a Hollow Sphere 
 
• Heat Transfer through a Composite Cylinder 
 
 
• Heat Transfer through a Composite Sphere 
 
 
• Critical Thickness of Insulation:  
o In case of cylinder, 
 
where, k 0 = Thermal conductivity, and h = Heat transfer coefficient 
o The drop in temperature across the wall and the air film will be proportional to their 
resistances, = hL/k. 
  
 
• Steady Flow of Heat along a Rod Circular fin 
?=pd 
 
 
• Generalized Equation for Fin Rectangular fin 
 
• Heat balance equation if A c constant and A s 8 P(x) linear 
 
• General equation of 2
nd
 order 
? = c1e
mx
 + c2e
-mx
 
o Heat Dissipation from an Infinitely Long Fin (l ? 8) 
 
? Heat transfer by conduction at base 
 
o Heat Dissipation from a Fin Insulated at the End Tip 
 
 
o Heat Dissipation from a Fin loosing Heat at the End Tip 
Page 5


Short notes for Heat transfer 
Fo u r ie r ’s Law of Heat Conduction 
 
• Q = Heat transfer in given direction. 
• A = Cross-sectional area perpendicular to heat flow direction. 
• dT = Temperature difference between two ends of a block of thickness dx 
• dx = Thickness of solid body 
•  = Temperature gradient in direction of heat flow. 
General Heat Conduction Equation 
• Carterisan Coordinates (side parallel to x, y and z-directions) 
 
       q g = Internal heat generation per unit volume per unit time 
       t = Temperature at left face of differential control volume 
       k x, k y, k z = Thermal conductivities of the material in x, y and z-directions respectively 
       c = Specific heat of the material 
       ? = Density of the material 
        a = Thermal diffusivity  
        dt = Instantaneous time. 
 
o For homogeneous and isotropic material 
 
o For steady state condition (P oi ss on ’s equation) 
 
o For steady state and absence of internal heat generation (Laplace equation) 
 
o For unsteady heat flow with no internal heat generation 
 
• Cylindrical Coordinates 
o For homogeneous and isotropic material, 
 
o For steady state unidirectional heat flow in radial direction with no internal heat 
generation, 
 
 
• Spherical Coordinates 
o For homogeneous and isotropic material 
 
o For steady state uni-direction heat flow in radial direction with no internal heat 
generation, 
 
• Thermal resistance of hollow cylinders  
 
 
  
• Thermal Resistance of a Hollow Sphere 
 
• Heat Transfer through a Composite Cylinder 
 
 
• Heat Transfer through a Composite Sphere 
 
 
• Critical Thickness of Insulation:  
o In case of cylinder, 
 
where, k 0 = Thermal conductivity, and h = Heat transfer coefficient 
o The drop in temperature across the wall and the air film will be proportional to their 
resistances, = hL/k. 
  
 
• Steady Flow of Heat along a Rod Circular fin 
?=pd 
 
 
• Generalized Equation for Fin Rectangular fin 
 
• Heat balance equation if A c constant and A s 8 P(x) linear 
 
• General equation of 2
nd
 order 
? = c1e
mx
 + c2e
-mx
 
o Heat Dissipation from an Infinitely Long Fin (l ? 8) 
 
? Heat transfer by conduction at base 
 
o Heat Dissipation from a Fin Insulated at the End Tip 
 
 
o Heat Dissipation from a Fin loosing Heat at the End Tip 
 
 
• Fin Efficiency 
• Fin efficiency is given by 
 
• If l ? 8 (infinite length of fin), 
 
 
• If finite length of fin, 
 
• Fin Effectiveness 
 
 
• Lumped Parameter System 
Q = - ? ? Ta T hA
dt
dT
VCp ? ? ?                     
? ?
? ?
?
dt
VCp
hA
Ta T
dT
? ) (
 
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FAQs on Heat Transfer Formulas for GATE ME Exam - Heat Transfer - Mechanical Engineering

1. What are the different modes of heat transfer?
Ans. The three modes of heat transfer are conduction, convection, and radiation. Conduction refers to the transfer of heat through direct contact between particles or molecules in a solid or stationary fluid. Convection involves the transfer of heat through the movement of a fluid (liquid or gas). Radiation is the transfer of heat through electromagnetic waves, which can occur in vacuum or through transparent media.
2. How can I calculate the rate of heat transfer through conduction?
Ans. The rate of heat transfer through conduction can be calculated using Fourier's law of heat conduction. The formula is given by Q = (k * A * ΔT) / d, where Q is the rate of heat transfer, k is the thermal conductivity of the material, A is the cross-sectional area, ΔT is the temperature difference, and d is the thickness of the material.
3. What is the formula for convective heat transfer coefficient?
Ans. The convective heat transfer coefficient (h) can be calculated using the formula h = (Q / A * ΔT), where Q is the rate of heat transfer, A is the surface area, and ΔT is the temperature difference between the surface and the surrounding fluid. The convective heat transfer coefficient depends on various factors such as the nature of the fluid, flow velocity, and surface roughness.
4. How can I determine the heat transfer by radiation?
Ans. The heat transfer by radiation can be determined using Stefan-Boltzmann's law. The formula is given by Q = ε * σ * A * (T₁⁴ - T₂⁴), where Q is the rate of heat transfer, ε is the emissivity of the material, σ is the Stefan-Boltzmann constant, A is the surface area, T₁ is the absolute temperature of the radiating surface, and T₂ is the absolute temperature of the surroundings.
5. What is the overall heat transfer coefficient?
Ans. The overall heat transfer coefficient (U) represents the combined effect of conduction, convection, and radiation in a system. It can be calculated using the formula 1/U = 1/h₁ + R + 1/h₂, where h₁ and h₂ are the convective heat transfer coefficients on either side of the solid surface, and R is the thermal resistance. The overall heat transfer coefficient determines the overall rate of heat transfer in a system involving multiple modes of heat transfer.
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