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22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2019

Question 7 of 8: Cooling rate of a molten weld droplet

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format: National Examination 16-Mec-A1 Applied Thermodynamics and Heat Transfer, 3 hours, open book. Eight questions of equal value: Part A — Thermodynamics (Q1–Q4) and Part B — Heat Transfer (Q5–Q8). A complete paper is any five questions (three from one part and two from the other).

Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — ideal-gas processes and entropy generation, polytropic compression, rigid-vessel charging, the reciprocating air compressor, throttling/flash separation, the steam turbine, and vapour-compression refrigeration/heat-pump cycles; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — steady radial conduction through a cylindrical wall with convection, conduction with uniform internal generation, transient (lumped) cooling by combined convection and radiation, and the effectiveness–NTU method for s​hell-and-tube exchangers. Steam and Freon-12 (R-12) properties are evaluated, which reproduces the IAPWS steam tables and the standard R-12 property tables to graphing accuracy; enthalpy differences (the only quantities used) are datum-independent. Air and combustion gases are treated as ideal with constant specific heats ($\gamma=1.4$, $R=0.287\ \text{kJ/kg}\cdot\text{K}$, $c_p=1.005$, $c_v=0.718\ \text{kJ/kg}\cdot\text{K}$).

Question 7 — Cooling rate of a molten weld droplet (Part B, equal value)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

QuantitySymbolValue
Diameter$D$0.5 mm
Initial temperature / velocity$T_i,\,V$1700 K, 1 m/s
Air temperature$T_\infty$300 K
Droplet $\rho,\,c_p,\,\epsilon$—2100 kg/m³, 1100 J/kg·K, 0.20
Air at film $T_f=1000$ K$k,\nu,Pr$0.0667 W/m·K, 1.20×10⁻⁴ m²/s, 0.726

Find. Instantaneous cooling rate $dT/dt$ (and the convective and radiative heat losses that drive it).

droplet 1700 K convection 0.455 W radiation 0.074 W V=1 m/s air T∞ = 300 K → dT/dt ≈ −3500 K/s
The tiny droplet is nearly isothermal (small Biot number), so a lumped energy balance applies. Convection dominates radiation ~6:1 at this size despite the 1700 K surface.

Approach. Get the convection coefficient from the Ranz–Marshall sphere correlation at the film temperature, sum the convective and radiative losses, and divide by the droplet's thermal capacitance to obtain the instantaneous cooling rate.

  1. Reynolds number and Nusselt (sphere). $Re=VD/\nu=(1)(5\times10^{-4})/1.20\times10^{-4}=4.16$; Ranz–Marshall: $$Nu=2+0.6\,Re^{1/2}Pr^{1/3}=2+0.6(2.04)(0.899)=3.10,\quad h=\frac{Nu\,k}{D}=\frac{3.10(0.0667)}{5\times10^{-4}}=414\ \text{W/m}^2\text{K}$$
  2. Convective and radiative losses. With $A=\pi D^2=7.854\times10^{-7}\ \text{m}^2$: $$\dot Q_\text{conv}=hA(T_i-T_\infty)=414(7.854\times10^{-7})(1400)=0.455\ \text{W}$$ $$\dot Q_\text{rad}=\epsilon\sigma A(T_i^4-T_\infty^4)=0.20(5.67\times10^{-8})(7.854\times10^{-7})(1700^4-300^4)=0.074\ \text{W}$$ $$\dot Q=\dot Q_\text{conv}+\dot Q_\text{rad}=\boxed{0.529\ \text{W}}$$
  3. Lumped cooling rate. With capacitance $\rho\,\forall\,c_p=2100\,(6.545\times10^{-11})\,1100=1.512\times10^{-4}\ \text{J/K}$ ($\forall=\pi D^3/6$): $$\frac{dT}{dt}=-\frac{\dot Q}{\rho\forall c_p}=-\frac{0.529}{1.512\times10^{-4}}=\boxed{-3.5\times10^{3}\ \text{K/s}}$$
QuantityResult
Convection coefficient414 W/m²K
Convective / radiative loss0.455 W / 0.074 W
Total heat loss0.529 W
Initial cooling rate≈ −3500 K/s