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Heat Transfer covers conduction, convection, radiation, thermal resistance networks, fins, and heat exchangers. Exams reward recognizing the governing mode and building the right resistance network before touching numbers — then executing correlations carefully. Full worked practice problems train both the setup judgment and the unit-heavy execution.

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Topics typically tested

  • 1-D steady conduction & thermal resistance
  • Fins & extended surfaces
  • Transient conduction (lumped capacitance)
  • Forced & natural convection correlations
  • Radiation exchange & view factors
  • Heat exchanger analysis (LMTD & NTU)

Sample Heat Transfer exam questions

Three original questions in the style of a real Heat Transfer exam, each with a worked solution. Your own practice exam can be built from your course's notes and syllabus.

Question 1Multiple choice1-D steady conduction & thermal resistance

A large plane wall consists of two layers in perfect thermal contact: 200 mm of brick with thermal conductivity 0.70 W/(m·K) on the inside and 50 mm of insulation with thermal conductivity 0.040 W/(m·K) on the outside. The indoor air is at 20 °C with a convection coefficient of 10 W/(m²·K) on the inner surface, and the outdoor air is at −10 °C with a convection coefficient of 25 W/(m²·K) on the outer surface. Under steady conditions, and neglecting radiation, what is the heat flux through the wall?

  1. A.

    17.9 W/m²

  2. B.

    19.5 W/m²

  3. C.

    24.0 W/m²

  4. D.

    105 W/m²

Worked solution
Answer:A

Steady one-dimensional conduction through layers in series, with convection at each face, is a series thermal-resistance network. Per unit area:

Rconv,in′′=1hin=110=0.100,Rbrick′′=Lk=0.2000.70=0.286R''_{conv,in} = \frac{1}{h_{in}} = \frac{1}{10} = 0.100,\qquad R''_{brick} = \frac{L}{k} = \frac{0.200}{0.70} = 0.286 Rins′′=0.0500.040=1.250,Rconv,out′′=125=0.040(all in m2⋅K/W)R''_{ins} = \frac{0.050}{0.040} = 1.250,\qquad R''_{conv,out} = \frac{1}{25} = 0.040\qquad(\text{all in m}^2\cdot\text{K/W})

Total: Rtot′′=0.100+0.286+1.250+0.040=1.676 m2⋅K/WR''_{tot} = 0.100 + 0.286 + 1.250 + 0.040 = 1.676\,\text{m}^2\cdot\text{K/W}.

The overall temperature difference drives the flux through the whole network:

q′′=Tin−ToutRtot′′=20−(−10)1.676=17.9 W/m2q'' = \frac{T_{in} - T_{out}}{R''_{tot}} = \frac{20 - (-10)}{1.676} = 17.9\,\text{W/m}^2

Because the same flux crosses every resistance, the intermediate temperatures follow at once: the inner wall surface is at Ts,in=20−17.9(0.100)=18.2T_{s,in} = 20 - 17.9(0.100) = 18.2 °C and the brick–insulation interface is at Tint=18.2−17.9(0.286)=13.1T_{int} = 18.2 - 17.9(0.286) = 13.1 °C. The insulation, which holds three-quarters of the total resistance, takes most of the temperature drop (about 22 °C), as expected.

The tempting answer 19.5 W/m² omits the two convection resistances; they are small here but not negligible (8% of the total). 24.0 W/m² uses the insulation alone and 105 W/m² the brick alone.

q′′=17.9 W/m2q'' = 17.9\,\text{W/m}^2 (from inside to outside)

Question 2Short answerTransient conduction (lumped capacitance)

A solid copper sphere of diameter 10 mm is initially at a uniform temperature of 150 °C. It is suddenly immersed in a large bath of oil at 30 °C, with a convection coefficient of 200 W/(m²·K) between the sphere and the oil. Copper properties: density 8933 kg/m³, specific heat 385 J/(kg·K), thermal conductivity 400 W/(m·K). Show that the lumped-capacitance method is valid, and find the time for the sphere's temperature to fall to 50 °C.

Worked solution
Answer:

Bi ≈ 8 × 10⁻⁴ (lumped analysis valid); t ≈ 51 s

Validity: the lumped method applies when the Biot number based on the characteristic length Lc=V/AsL_c = V/A_s is below 0.1. For a sphere Lc=ro/3L_c = r_o/3:

Lc=0.0053=1.667×10−3 m,Bi=hLck=200(1.667×10−3)400=8.3×10−4L_c = \frac{0.005}{3} = 1.667 \times 10^{-3}\,\text{m},\qquad Bi = \frac{hL_c}{k} = \frac{200(1.667 \times 10^{-3})}{400} = 8.3 \times 10^{-4}

Bi≪0.1Bi \ll 0.1, so internal conduction is so fast compared with surface convection that the sphere stays essentially uniform in temperature, and the lumped energy balance ρcV dT/dt=−hAs(T−T∞)\rho c V\,dT/dt = -hA_s(T - T_\infty) applies.

Its solution is an exponential decay with time constant τ=ρcV/(hAs)=ρcLc/h\tau = \rho c V/(hA_s) = \rho c L_c/h:

τ=8933(385)(1.667×10−3)200=28.66 s\tau = \frac{8933(385)(1.667 \times 10^{-3})}{200} = 28.66\,\text{s} T−T∞Ti−T∞=e−t/τ  ⇒  50−30150−30=16=e−t/28.66\frac{T - T_\infty}{T_i - T_\infty} = e^{-t/\tau} \;\Rightarrow\; \frac{50 - 30}{150 - 30} = \frac{1}{6} = e^{-t/28.66} t=28.66 ln⁡6=28.66(1.792)=51.4 st = 28.66\,\ln 6 = 28.66(1.792) = 51.4\,\text{s}

The sphere loses five-sixths of its initial temperature excess in about 1.8 time constants, which is the expected behaviour for exponential cooling (one time constant removes 63% of the excess, two remove 86%).

Bi≈8×10−4Bi \approx 8 \times 10^{-4}, so lumped analysis is valid; t≈51 st \approx 51\,\text{s}

Question 3Worked problemHeat exchanger analysis (LMTD & NTU)

A counterflow double-pipe heat exchanger is used to cool oil with water. Oil (cp=2100c_p = 2100 J/(kg·K)) flows at 0.50 kg/s and must be cooled from 120 °C to 60 °C. Cooling water (cp=4180c_p = 4180 J/(kg·K)) enters at 20 °C with a flow rate of 0.40 kg/s. The overall heat transfer coefficient is U=300U = 300 W/(m²·K). Neglect heat loss to the surroundings. Find (a) the heat transfer rate, (b) the water outlet temperature, (c) the log mean temperature difference, and (d) the required heat transfer surface area.

Worked solution
Answer:

(a) 63.0 kW; (b) 57.7 °C; (c) 50.3 °C; (d) 4.17 m²

(a) The heat given up by the oil follows from an energy balance on the hot stream:

Q˙=m˙hcp,h(Th,in−Th,out)=0.50(2100)(120−60)=63 000 W=63.0 kW\dot Q = \dot m_h c_{p,h}(T_{h,in} - T_{h,out}) = 0.50(2100)(120 - 60) = 63\,000\,\text{W} = 63.0\,\text{kW}

(b) With no losses the water absorbs all of it:

Tc,out=Tc,in+Q˙m˙ccp,c=20+63 0000.40(4180)=20+37.7=57.7 ∘CT_{c,out} = T_{c,in} + \frac{\dot Q}{\dot m_c c_{p,c}} = 20 + \frac{63\,000}{0.40(4180)} = 20 + 37.7 = 57.7\,^\circ\text{C}

The water warms less than the oil cools because its capacity rate (m˙cp=1672\dot m c_p = 1672 W/K) exceeds the oil's (1050 W/K).

(c) In counterflow the hot inlet faces the cold outlet and the hot outlet faces the cold inlet, so the end temperature differences are

ΔT1=Th,in−Tc,out=120−57.7=62.3 ∘C,ΔT2=Th,out−Tc,in=60−20=40.0 ∘C\Delta T_1 = T_{h,in} - T_{c,out} = 120 - 57.7 = 62.3\,^\circ\text{C},\qquad \Delta T_2 = T_{h,out} - T_{c,in} = 60 - 20 = 40.0\,^\circ\text{C} ΔTlm=ΔT1−ΔT2ln⁡(ΔT1/ΔT2)=62.3−40.0ln⁡(62.3/40.0)=22.30.443=50.3 ∘C\Delta T_{lm} = \frac{\Delta T_1 - \Delta T_2}{\ln(\Delta T_1/\Delta T_2)} = \frac{62.3 - 40.0}{\ln(62.3/40.0)} = \frac{22.3}{0.443} = 50.3\,^\circ\text{C}

No correction factor is needed for a true counterflow double-pipe exchanger (F=1F = 1).

(d) From the rate equation Q˙=UA ΔTlm\dot Q = UA\,\Delta T_{lm}:

A=Q˙U ΔTlm=63 000300(50.3)=4.17 m2A = \frac{\dot Q}{U\,\Delta T_{lm}} = \frac{63\,000}{300(50.3)} = 4.17\,\text{m}^2

The log mean (50.3 °C) lies between the two end differences and slightly below their arithmetic mean (51.2 °C), as it always does. A parallel-flow arrangement with the same four temperatures would give a log mean of only 26.0 °C and need almost twice the area.

(a) 63.0 kW; (b) Tc,out=57.7T_{c,out} = 57.7 °C; (c) ΔTlm=50.3\Delta T_{lm} = 50.3 °C; (d) A=4.17 m2A = 4.17\,\text{m}^2

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