Skip to content
Sahithyan's S3
1
Sahithyan's S3 — Engineering Thermodynamics

Heat Transfer

The movement of thermal energy due to temperature difference. Heat flows from higher temperature to lower temperature.

Three modes: conduction, convection, radiation. Heat transfer mode depends on the medium (solid, fluid, or vacuum).

Heat transfer due to random motion of atoms or molecules. Occurs in solids and stationary fluids.

q˙=kdTdx\dot{q} = -k \frac{dT}{dx}
  • q˙\dot{q}: heat flux
  • kk: thermal conductivity
  • dTdx\frac{dT}{dx}: temperature gradient

Larger kk → faster heat transfer.

Rate of heat transfer per unit area. Denoted by q˙\dot{q}. Unit: Wm2\text{W}\,\text{m}^{-2}.

Measure of a material’s ability to conduct heat. Denoted by kk. Unit: Wm1K1\text{W}\,\text{m}^{-1}\,\text{K}^{-1}.

Heat transfer from a solid surface to a moving fluid next to the surface (or vice versa).

Can be caused by either:

  • Advection: bulk fluid motion.
  • Diffusion: random fluid movement.

2 types:

  • Natural convection: buoyancy-driven flow.
  • Forced convection: external forcing (fan, pump).
q˙=h(TsT)\dot{q} = h (T_s - T_\infty)
  • q˙\dot{q}: convective heat flux
  • hh: heat transfer coefficient
  • TsT_s: surface temperature
  • TT_\infty: fluid temperature

Measure of convective heat transfer between surface and fluid. Denoted by hh. Unit: Wm2K1\text{W}\,\text{m}^{-2}\,\text{K}^{-1}.

Varies with flow conditions.

Heat transfer through electromagnetic waves. No medium required. Wavelength range: about 0.1–100 μm. Depends on surface temperature and emissivity. Dominant at high temperatures or between large surfaces.

q˙=σεσf(T14T24)\dot{q} = \sigma \varepsilon \sigma f (T_1^4 - T_2^4)

Here:

  • q˙\dot{q}: net radiative heat flux
  • σ\sigma: Stefan-Boltzmann constant
  • ε\varepsilon: emissivity
  • ff: geometrical factor

Denoted by σ\sigma. Value: 5.67×108  Wm2K45.67 \times 10^{-8} \;\text{W}\,\text{m}^{-2}\,\text{K}^{-4}.

Measure of a surface’s ability to emit thermal radiation. Denoted by ε[0,1]\varepsilon \in [0,1].

  • ε=0\varepsilon=0: perfect reflector
  • ε=1\varepsilon=1: perfect emitter, blackbody

Depends on the orientation and shape of the surfaces exchanging radiation.

Used for walls, rods, slabs where temperature varies in only one direction.

dQdx=ddx(kdTdx)=0\frac{dQ}{dx} = \frac{d}{dx} \left(k \frac{dT}{dx}\right) = 0 d2Tdx2+(1AdAdx)dTdx=0\frac{d^2 T}{dx^2} + \left( \frac{1}{A} \frac{\text{d}A}{\text{d}x} \right) \frac{\text{d}T}{\text{d}x} = 0

For constant AA:

d2Tdx2=0\frac{d^2 T}{dx^2} = 0

For a plane slab, WAA is constant w.r.t xx. Integrating the above equation twice gives:

T(x)=ax+bT(x) = a x + b

Temperature varies linearly throughout the conduction direction.

T(x)=T1+T2T1LxT(x) = T_1 + \frac{T_2 - T_1}{L}x

Conduction–convection systems can be modeled using electrical analogy.

R=ΔTQR = \frac{\Delta T}{Q}

For a composite wall series and parallel thermal resistances are combined similar to electrical resistances.

Rcond=LkAR_\text{cond} = \frac{L}{kA} Rconv=1hAR_\text{conv} = \frac{1}{hA}