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Materials Science · Heat transport, expansion and thermal response

Interfaces, insulation and thermal management

Useful background: Energy, stability and environmental context; Measuring and checking material claims. Each worked case explains the quantities it uses.

Back to the chapter

After reading, you can

  • Assess thermal pathways through complete layered systems.
  • Convert a complete steady heat path into thermal resistances with the correct units and boundary conditions.
  • Distinguish series heat-rate continuity from parallel heat splitting.
  • Compare source cooling and protection of a neighbouring zone under the same fixed heat input.
  • Identify which extra temperatures or heat-rate evidence distinguish competing explanations of an improvement.
01

The heat path includes interfaces

A heat spreader can have high conductivity but still perform poorly if contact to the source is weak. Layers, gaps and interfaces add thermal resistance. For a simple steady series path, layer resistances L/(kA) add together with relevant contact resistances.

A warmer source and a neighbouring temperature-sensitive zone can need opposite changes: conduct energy readily towards a sink, but limit transfer into the protected zone. Insulating every route can protect the neighbour while making the source hotter. Start by drawing where energy enters, where it can leave, and which temperatures matter.

The original qualitative figure shows successive layers. The new comparison adds a second route and two simultaneous temperature requirements. All values below are original hypothetical teaching inputs, not measurements, material specifications or operating limits for real equipment.

02

A resistance relates a temperature drop to a heat rate

For a stated steady path define thermal resistance R = ΔT/Q̇, where Q̇ is the heat rate in watts and ΔT is the warmer-side minus cooler-side temperature difference. Its unit is K/W. A temperature difference of 1 K equals a difference of 1 °C; absolute kelvin temperatures are needed in radiation laws. R is not thermal conductivity k, whose unit is W/(m K).

For a uniform plane layer with thickness L, constant directional k, cross-sectional area A and one-dimensional steady conduction without internal heat generation, Q̇ = kAΔT/L. Rearranging gives R_layer = L/(kA). For example, L = 2.00 mm, k = 100 W/(m K) and A = 40.0 mm² = 4.00 × 10⁻⁵ m² give R_ℓ = 0.500 K/W. This is a short uniform bulk link in our model. A real spreader’s lateral redistribution and nonuniform source area can require a two- or three-dimensional model rather than this slab formula.

A whole contact resistance R_c includes the specified interface and has units K/W. Real surfaces meet over a distribution of spots and gaps; pressure, surface shape, intervening material, gas and temperature can change the transfer. A filler can improve coupling while also adding its own thickness resistance. Do not count the same layer or contact twice. An area-specific resistance in m² K/W is a different quantity; Lattice vibrations, electrons and heat transport develops the microscopic and interface distinction.

For an isothermal surface exchanging heat with a specified fluid, a bounded convection model writes Q̇ = hA_s(T_surface − T_fluid). The resulting R_h = 1/(hA_s) uses exposed surface area A_s, which need not equal the layer’s conduction area A. The coefficient h depends on the flow, fluid, geometry and state; it is not the solid’s conductivity. Here hA_s is supplied as 2/3 W/K, so R_h = 1.50 K/W. We do not calculate a real fin efficiency or airflow.

Elements are in series when the same steady heat rate passes through each, with no branch, generation or storage between them. Then ΔT_total = Q̇(R₁ + R₂ + …). Distinct parallel paths between the same temperature nodes instead share ΔT and carry rates that add: Q̇_total = ΔT(1/R₁ + 1/R₂ + …). Heat rate, not necessarily heat flux per area, is conserved through elements with different areas.

03

One source feeds a cooling route and a protected zone

Stipulate a source S receiving constant power P = 10.0 W and an ambient reservoir held at T₀ = 25.0 °C. Treat S and a neighbouring zone Z as uniform-temperature nodes. Z has no heat generation. The primary cooling route goes from S through R_c = 4.00 K/W, the bulk link R_ℓ = 0.500 K/W and the surface-to-fluid resistance R_h = 1.50 K/W. Its total is R_m = 6.00 K/W.

The second route goes from S through insulation resistance R_i = 12.0 K/W into Z, then through R_z = 4.00 K/W to the same ambient reservoir. Its total from S to ambient is R_b = R_i + R_z = 16.0 K/W. The diagram is a thermal network, not a spatial drawing or an assertion that all these paths have equal area. All resistances are supplied positive constants for the temperatures considered, 25–85 °C; no other heat paths, radiation, storage or temperature-dependent power are included.

Write θ_s = T_s − T₀ and θ_z = T_z − T₀ for temperature rises. The primary heat rate is Q̇_m = θ_s/R_m. At Z, steady balance requires Q̇_z = (θ_s − θ_z)/R_i = θ_z/R_z. Consequently θ_z = θ_s R_z/(R_i + R_z), and the branch rate is Q̇_z = θ_s/R_b. At S, P = Q̇_m + Q̇_z. No source energy disappears into a resistance; all 10.0 W eventually reaches the reservoir.

Solving these balances gives θ_s = P/(1/R_m + 1/R_b) and θ_z = P R_m R_z/(R_m + R_b). The baseline values are θ_s = 43.6364 K and θ_z = 10.9091 K, so T_s = 68.6364 °C and T_z = 35.9091 °C. Heat rates are Q̇_m = 7.27273 W and Q̇_z = 2.72727 W. They sum to P; do not send 10.0 W through each parallel route.

Within the primary series route, those 7.27273 W give contact, bulk and fluid-boundary drops of 29.0909, 3.63636 and 10.9091 K. Their sum is θ_s. The largest baseline share lies at the contact. This allocation is specific to the whole path and current heat split, not a ranking of every possible interface or material.

Two routes share the fixed source inputOriginal hypothetical two-node steady thermal network, not a spatial drawing or experimental apparatus. A source S receives fixed 10.0 watts and is at 68.6364 degrees Celsius in the baseline model. Its primary route to the 25.0 degree ambient has contact resistance 4.00, uniform bulk-link resistance 0.500 and fluid-boundary resistance 1.50 kelvins per watt in series, total 6.00. It carries 7.27273 watts. A second route goes through insulation resistance 12.0 kelvins per watt into zone Z at 35.9091 degrees Celsius and then through resistance 4.00 kelvins per watt to the same ambient, total 16.0. It carries 2.72727 watts. Z generates no heat. The primary path is shown on the left and the zone path on the right; lines and arrows indicate connectivity and positive heat direction, not physical length, cross-section or a trajectory. The lower zero-origin stacked power bar runs from zero to 10 watts at 50 pixels per watt. Solid blue is the 7.27273 watt primary rate and orange hatching is the 2.72727 watt zone rate. These add to the fixed 10.0 watt input. The model excludes all other paths, storage and radiation, uses one fixed reservoir and constant supplied resistances; no real design is qualified.A source can feed two thermal objectivesBaseline: P = 10.0 W; all R in K/WSource ST_s = 68.6364 °CContact R_c4.00Insulation R_i12.0Bulk link R_ℓ0.500Zone Z; no generationT_z = 35.9091 °CFluid boundary R_h1.50Zone to ambient R_z4.00Common fixed ambient: T₀ = 25.0 °CBoth paths ultimately reach this reservoirSteady input power is divided, not duplicated0246810Heat rate (W)Solid: primary 7.27273 WHatched: through Z 2.72727 WNo spatial or material-property scale is implied.
Original hypothetical two-node steady thermal network, not a spatial drawing or experimental apparatus. A source S receives fixed 10.0 watts and is at 68.6364 degrees Celsius in the baseline model. Its primary route to the 25.0 degree ambient has contact resistance 4.00, uniform bulk-link resistance 0.500 and fluid-boundary resistance 1.50 kelvins per watt in series, total 6.00. It carries 7.27273 watts. A second route goes through insulation resistance 12.0 kelvins per watt into zone Z at 35.9091 degrees Celsius and then through resistance 4.00 kelvins per watt to the same ambient, total 16.0. It carries 2.72727 watts. Z generates no heat. The primary path is shown on the left and the zone path on the right; lines and arrows indicate connectivity and positive heat direction, not physical length, cross-section or a trajectory. The lower zero-origin stacked power bar runs from zero to 10 watts at 50 pixels per watt. Solid blue is the 7.27273 watt primary rate and orange hatching is the 2.72727 watt zone rate. These add to the fixed 10.0 watt input. The model excludes all other paths, storage and radiation, uses one fixed reservoir and constant supplied resistances; no real design is qualified.
04

Compare what changes and what stays fixed

Compare changes at the same P, ambient, geometry outside the changed element and stated resistance laws. Doubling only the bulk link’s k changes R_ℓ from 0.500 to 0.250 K/W. It does not alter the contact, exposed-fluid area or bypass. The primary total falls only from 6.00 to 5.75 K/W. Re-solving the split gives T_s = 67.2989 °C and T_z = 35.5747 °C. The source-to-ambient rise falls about 3.07%, not by half.

Alternatively, supply an improved contact R_c = 1.00 K/W while leaving everything else at baseline. Now R_m = 3.00 K/W. The source is cooler, T_s = 50.2632 °C, and Z also becomes cooler, T_z = 31.3158 °C. The primary route carries more heat, 8.42105 W. Its fluid-facing surface therefore rises 12.6316 K above ambient, more than the baseline 10.9091 K, even while the source cools. A warmer sink surface need not mean worse source cooling.

Increasing only R_i from 12.0 to 28.0 K/W instead reduces heat entering Z: T_z becomes the same 31.3158 °C, but T_s rises to 75.5263 °C. The primary path must now remove more of the fixed input. A protected-zone temperature alone cannot distinguish this change from the improved-contact case, and calling either change simply better hides the second objective.

Combining R_c = 1.00 with R_i = 28.0 K/W yields T_s = 52.4286 °C and T_z = 28.4286 °C. Relative to contact improvement alone, Z is cooler but S is slightly warmer. That is a trade between two specified outcomes, not a contradiction of energy conservation.

Original exact fixed-10.0-W comparisons, rounded for display. Each row changes only the named baseline inputs; these are hypothetical network responses.
ChangeR_m (K/W)R_b (K/W)T_s (°C)T_z (°C)
Baseline6.0016.068.636435.9091
Double bulk k only5.7516.067.298935.5747
Contact R_c = 1.003.0016.050.263231.3158
Insulation R_i = 28.06.0032.075.526331.3158
Both contact and insulation changes3.0032.052.428628.4286
05

A change must satisfy both chosen requirements

For this exercise alone, declare two inclusive comparison screens: T_s ≤ 60.0 °C and T_z ≤ 32.0 °C at the stated 25.0 °C ambient. These are invented task criteria, not real equipment ratings or a safety margin. Baseline and the bulk-k change fail both. The insulation-only change meets the Z screen but fails the source screen. Contact improvement alone and the combined change meet both within the model.

The two-panel graph varies R_i from 8.00 to 40.0 K/W while preserving P = 10.0 W, R_z = 4.00 and either R_m = 6.00 or 3.00 K/W. Increasing insulation raises θ_s = P R_m(R_i + R_z)/(R_m + R_i + R_z), while lowering θ_z = P R_m R_z/(R_m + R_i + R_z). A fixed source power is essential to that opposing trend. If a thermostat instead fixes T_s, the required P and branch rates change; it is a different boundary problem.

With the improved R_m = 3.00, θ_s always stays below 30.0 K for positive R_i. The Z requirement gives 120/(R_i + 7) ≤ 7, or R_i ≥ 71/7 = 10.1429 K/W. Thus the tested range meets both screens from that value through 40.0 K/W. With baseline R_m = 6.00, no choice of positive R_i can meet both at 10.0 W: the two permitted heat-removal rates cannot sum that high.

To see the last point without searching a curve, the source screen permits at most 35/6 = 5.83333 W through the baseline primary path. The Z screen permits at most 7/4 = 1.750 W from Z to ambient. Their sum is 91/12 = 7.58333 W. At 10.0 W, insulation changes alone cannot satisfy both. This bound uses the stated two-path topology and both specified temperatures; a new path, changed ambient, heat generation in Z or temperature-dependent resistance requires a new account.

Insulation can protect a zone while warming the sourceOriginal calculated model families at fixed power 10.0 watts, ambient 25.0 degrees Celsius, zone-to-ambient resistance 4.00 kelvins per watt and insulation R_i from 8.00 to 40.0 kelvins per watt. The horizontal scale in both panels is 15 pixels per kelvin per watt. Solid blue curves with circle markers use baseline primary resistance R_m equals 6.00 kelvins per watt. Dashed violet curves with square markers use improved R_m equals 3.00. The upper vertical axis is source temperature from 40 to 85 degrees Celsius at 8 pixels per degree. Both source curves rise as insulation increases; the dashed orange comparison screen is 60 degrees Celsius. The lower axis is protected-zone temperature from 25 to 42 degrees Celsius at 20 pixels per degree. Both zone curves fall as insulation increases; its dashed orange comparison screen is 32 degrees Celsius. Markers at R_i equals 12 and 28 correspond to table comparisons, not measurements. A hollow diamond on the improved zone curve marks R_i equals 71/7, approximately 10.1429, where the zone is exactly 32 degrees. In that improved family the source stays below 55 degrees, so tested R_i at or above that threshold meets both invented screens. No member of the baseline family can meet both at 10 watts. The two panels have different vertical scales; the limits are stipulated comparison criteria, not material ratings, safety limits or uncertainty bands.One change can move two temperatures oppositelyFixed P = 10.0 W; T₀ = 25.0 °C; R_z = 4.00 K/WR_m = 6.00 K/W: solid / circlesR_m = 3.00 K/W: dashed / squaresSource T_s (°C)40506070808581624324060 °C screenInsulation R_i (K/W)Protected zone T_z (°C)25283236404281624324032 °C screenR_i = 10.1429Insulation R_i (K/W)Improved path: R_i ≥ 10.1429 K/W meets both screens.
Original calculated model families at fixed power 10.0 watts, ambient 25.0 degrees Celsius, zone-to-ambient resistance 4.00 kelvins per watt and insulation R_i from 8.00 to 40.0 kelvins per watt. The horizontal scale in both panels is 15 pixels per kelvin per watt. Solid blue curves with circle markers use baseline primary resistance R_m equals 6.00 kelvins per watt. Dashed violet curves with square markers use improved R_m equals 3.00. The upper vertical axis is source temperature from 40 to 85 degrees Celsius at 8 pixels per degree. Both source curves rise as insulation increases; the dashed orange comparison screen is 60 degrees Celsius. The lower axis is protected-zone temperature from 25 to 42 degrees Celsius at 20 pixels per degree. Both zone curves fall as insulation increases; its dashed orange comparison screen is 32 degrees Celsius. Markers at R_i equals 12 and 28 correspond to table comparisons, not measurements. A hollow diamond on the improved zone curve marks R_i equals 71/7, approximately 10.1429, where the zone is exactly 32 degrees. In that improved family the source stays below 55 degrees, so tested R_i at or above that threshold meets both invented screens. No member of the baseline family can meet both at 10 watts. The two panels have different vertical scales; the limits are stipulated comparison criteria, not material ratings, safety limits or uncertainty bands.
06

A cooler source does not identify which element improved

Consider a separate invented comparison at the same baseline P, R_i, R_z, R_ℓ and ambient. Suppose the primary total is now R_m = 5.00 K/W. Hypothesis A changes only R_c from 4.00 to 3.00 K/W and retains R_h = 1.50. Hypothesis B retains R_c = 4.00 but changes R_h from 1.50 to 0.500 K/W. Both have the same series sum.

Both predict T_s = 63.0952 °C, T_z = 34.5238 °C and Q̇_m = 7.61905 W. Even perfect observations of those two node temperatures do not distinguish the two supplied explanations. The interface drop and the fluid-facing surface temperature do differ: A gives ΔT_c = 22.8571 K and T_face = 36.4286 °C; B gives ΔT_c = 30.4762 K and T_face = 28.8095 °C.

Temperature information on both sides of the contact, combined with independently established heat through that contact, can therefore challenge the contact explanation. A fluid-facing temperature and the actual fluid condition constrain the other explanation. Placement, calibration, sensor contact, spatial gradients and uncertainty matter. A nominal fan setting is not a measurement of h, and total source power is not automatically the heat through one branch.

Use evidence at changed conditions as well: a repeated result at another power or ambient can challenge constant-resistance and unchanged-path assumptions. A fitted source-to-ambient resistance alone can hide changed contact, airflow, bypass, radiative exchange or input power. Calibration, uncertainty and repeatability develops the measurement account; a successful fit does not uniquely establish the microscopic mechanism.

Two original conditional explanations with identical source/zone temperatures and primary heat rate. Internal temperature evidence separates their predictions.
ExplanationR_c (K/W)R_h (K/W)Contact drop (K)Fluid-facing T (°C)
A: contact change3.001.5022.857136.4286
B: boundary change4.000.50030.476228.8095
07

Management may require opposite functions

An insulator limits transfer; a spreader redistributes heat; a heat sink transfers it to surroundings. Material conductivity alone cannot select the whole design. Include convection, radiation, area, interface condition and operating temperature.

A finite heat sink first stores some input energy, but its heat capacity is not an unlimited steady removal rate. Our steady model assumes that storage has ended and the reservoir remains at 25.0 °C. It predicts no warm-up time, pulse peak or thermal stress. Heat capacity and thermal conductivity and Thermal diffusivity and response times develop the distinct storage and timescale questions; Thermal expansion and thermal stress follows mechanical consequences.

Convection changes with fluid motion and surface geometry. Radiation can provide another route, depending on absolute temperatures, surface optical properties and which surfaces exchange energy. It cannot always be represented by one temperature-independent K/W value. These effects were excluded, not proved absent, in the numerical network. Insulation that reduces conduction may leave a radiative or structural bridge, so its material k alone does not determine complete protection.

Finally, a real spreader need not be isothermal. A local hot region, an unequal contact area or a poorly connected path may defeat a lumped node picture. Verify the heat paths, source power, temperatures and operating conditions before treating a component comparison as a material claim. Meeting the invented two-temperature screens supplies neither uncertainty margin, reliability nor qualification of an actual design.

Thermal resistances share a heat pathHeat travels through successive layers and interfaces from a hot boundary to a cold one. Each resistance contributes to the temperature drop under the stated steady series model.HotColdLayers + interfaces + boundary heat transfer
Heat travels through successive layers and interfaces from a hot boundary to a cold one. Each resistance contributes to the temperature drop under the stated steady series model.

Worked examples

Work through the case

A thin gap dominates a stack’s thermal resistance. Will doubling the spreader conductivity necessarily halve total resistance?

  1. Separate layer and gap contributions.
  2. Only the spreader’s contribution is reduced.
  3. Add the unchanged dominant resistance.

No. Improving a small contribution may barely change the total.

Close the heat balance before allocating drops

For the baseline 10.0 W source, calculate both branch heat rates and the three primary-path temperature drops. Why is it wrong to send all 10.0 W through R_c?

  1. The source sees two complete routes to the same ambient: R_m = 4.00 + 0.500 + 1.50 = 6.00 K/W and R_b = 12.0 + 4.00 = 16.0 K/W.
  2. θ_s = 10.0/(1/6 + 1/16) = 43.6364 K. Then Q̇_m = θ_s/6 = 7.27273 W and Q̇_z = θ_s/16 = 2.72727 W. Their sum is 10.0 W.
  3. Only Q̇_m crosses R_c, R_ℓ and R_h. Their drops are 29.0909, 3.63636 and 10.9091 K; adding them recovers θ_s.
  4. The zone rise is Q̇_zR_z = 10.9091 K. The insulation drop is Q̇_zR_i = 32.7273 K, so the bypass also sums to θ_s.

The 10.0 W splits into 7.27273 and 2.72727 W. Contact drop is 29.0909 K, not 40.0 K; heat-rate continuity applies within a series branch, not across both parallel branches separately.

One improved temperature can hide a worse second outcome

Compare contact-only R_c = 1.00 and insulation-only R_i = 28.0 K/W against the two invented screens. Everything else remains at baseline. Does their identical T_z identify the change?

  1. Contact improvement gives complete routes 3.00 and 16.0 K/W. The rises are θ_s = 25.2632 K and θ_z = 6.31579 K. Both screens are met.
  2. Insulation improvement gives routes 6.00 and 32.0 K/W. The rises are θ_s = 50.5263 K and θ_z = 6.31579 K. Only the Z screen is met.
  3. The same θ_z means the same Q̇_z = θ_z/4 = 1.57895 W. It does not mean the same source temperature or same complete-path resistance.
  4. Fixed power forces the remaining 8.42105 W through the primary route in either case; its resistance is 3.00 versus 6.00 K/W.

Both changes give T_z = 31.3158 °C, but source temperatures are 50.2632 and 75.5263 °C. A protected-zone temperature alone does not identify which path changed or establish both requirements.

Choose an observation that separates two explanations

For the two R_m = 5.00 K/W explanations, calculate the common primary heat rate, the contact drop and the fluid-facing temperature. Which observation could distinguish A from B?

  1. Both total routes are 5.00 and 16.0 K/W. θ_s = 10.0/(1/5 + 1/16) = 38.0952 K, Q̇_m = θ_s/5 = 7.61905 W and θ_z = 9.52381 K.
  2. A: ΔT_c = (7.61905)(3.00) = 22.8571 K and T_face = 25.0 + (7.61905)(1.50) = 36.4286 °C.
  3. B: ΔT_c = (7.61905)(4.00) = 30.4762 K and T_face = 25.0 + (7.61905)(0.500) = 28.8095 °C.
  4. A contact-spanning temperature difference with independent branch heat, or the appropriately located surface/fluid temperatures, separates these ideal predictions. Real measurements require uncertainty and placement assessment.

The source/zone observations coincide, but contact drop and fluid-facing temperature do not. Measure a discriminating internal quantity rather than fitting the same total again.

Find what insulation alone cannot achieve

Keep baseline R_m = 6.00 and R_z = 4.00 K/W but allow positive R_i to vary. What maximum fixed P can meet the invented T_s ≤ 60.0 and T_z ≤ 32.0 °C screens at 25.0 °C ambient? Is the bound attainable within this model?

  1. The permitted source rise is 35.0 K, so the primary route removes at most 35/6 = 5.83333 W. The zone’s 7.00 K rise permits at most 7/4 = 1.750 W.
  2. Adding the two maxima gives P ≤ 5.83333 + 1.750 = 7.58333 W = 91/12 W. No change of R_i can make those two routes remove 10.0 W while respecting both temperatures.
  3. To reach the bound, both temperatures must reach their screens. The insulation then spans 35 − 7 = 28 K at 1.750 W, requiring R_i = 28/1.750 = 16.0 K/W.
  4. This positive value closes both node balances, so the bound is attained for the exact invented model. It is not a real allowable power or margin.

The model maximum is 7.58333 W, attained at R_i = 16.0 K/W with both comparison screens at equality. The original 10.0 W task needs a change beyond insulation alone.

Try the reasoning

  1. Can contact pressure affect heat transfer?

    Show the answer and reasoning

    Yes.

    It changes contact and gap structure.

  2. Does a heat spreader remove energy by itself?

    Show the answer and reasoning

    No.

    The complete path must transfer energy to a sink or surroundings.

  3. At the same original 10.0 W input, only bulk k doubles. What happens to the total source-to-ambient temperature rise, and why does a contact drop actually increase slightly?

    Show the answer and reasoning

    The source rise falls from 43.6364 to 42.2989 K, about 3.07%. The contact drop rises from 29.0909 to 29.4253 K.

    R_ℓ halves, but the dominant contact and the other paths remain. The primary route becomes easier and carries 7.35632 W rather than 7.27273 W; multiplying that larger branch rate by unchanged R_c = 4.00 gives the slightly larger contact drop. A drop depends on both resistance and branch heat rate.

  4. Retain every baseline resistance and ambient, but supply P = 6.00 W. Find T_s and T_z and apply the same two invented screens.

    Show the answer and reasoning

    T_s = 51.1818 °C and T_z = 31.5455 °C; both screens are met within the supplied model.

    The linear network’s rises scale by 6/10: 26.1818 and 6.54545 K. Add ambient to each. The source input changed; the result does not prove a new contact, conductivity or insulator.

  5. Keep the contact-only improvement R_c = 1.00 K/W and 10.0 W input, but change the common ambient to 35.0 °C. Assume the same supplied laws remain valid. Do the fixed 60.0/32.0 °C screens still pass?

    Show the answer and reasoning

    No. T_s = 60.2632 °C and T_z = 41.3158 °C, so both fixed screens fail.

    The unchanged linear network retains rises 25.2632 and 6.31579 K. Add the new ambient, not the old one. The relative improvements do not guarantee absolute temperature requirements at a changed environment.

  6. For improved R_m = 3.00 K/W, P = 10.0 W and the original ambient/R_z, find the least R_i in the tested 8–40 K/W range that meets both screens. Does R_i = 10.0 K/W suffice?

    Show the answer and reasoning

    The threshold is 71/7 = 10.1429 K/W. R_i = 10.0 does not suffice: T_z ≈ 32.0588 °C.

    θ_z = 120/(R_i + 7). Requiring θ_z ≤ 7 gives R_i ≥ 120/7 − 7. Source rise remains below 30 K throughout this positive-resistance family, so its 35 K screen adds no restriction. At R_i = 10, θ_z = 120/17 ≈ 7.05882 K.

  7. A different controller fixes T_s = 60.0 °C instead of supplying 10.0 W. Keep baseline R_m = 6.00 and R_z = 4.00 at 25.0 °C ambient. Compare R_i = 12.0 and 28.0 K/W. Does insulation now make the source hotter?

    Show the answer and reasoning

    T_s stays fixed. Required steady input falls from 8.02083 to 6.92708 W, while T_z falls from 33.750 to 29.375 °C.

    At θ_s = 35 K, the primary rate is 35/6 = 5.83333 W. Bypass rates are 35/16 = 2.18750 and 35/32 = 1.09375 W. Add rates to obtain the input the controller must supply; multiply bypass by R_z for zone rise. This is a changed boundary condition, not the original fixed-power experiment.

  8. Measured steady source temperatures are below the two-path model prediction. Does that prove R_c is smaller? Name a distinct explanation and an observation that can test it.

    Show the answer and reasoning

    No. An omitted heat path, lower actual source power or a changed fluid/radiative boundary can also lower the temperature.

    For example, independently establish actual input power and branch heat flows, or measure across the contact and at the fluid-facing surface. A lower fitted total resistance alone does not identify the changed element. A transient reading also cannot be compared as though steady storage were zero.

What to carry forward

  • Follow the entire heat path.
  • Improve the resistance that actually limits performance.
  • Use K/W for a whole resistance and preserve its area and boundary meaning.
  • Series elements share a heat rate; parallel paths share a temperature difference and divide the heat rate.
  • Cooling a source and insulating a neighbour are different objectives under the same energy balance.
  • A changed internal temperature can distinguish explanations that give the same terminal response.

References

Teaching resources and research supporting this lesson’s explanations and examples.

  1. College Physics 2e · 14.5 ConductionOpenStaxTextbook sectionopenstax.orgRead source
  2. Massachusetts Institute of Technology3 sources
    1. Materials Processing · Lecture 1: What is Materials Processing?Chris Schuh / MIT OpenCourseWareCourse notes · PDFocw.mit.eduRead source
    2. 16.4 Thermal Resistance CircuitsMIT Unified Engineering · Thermodynamics and PropulsionSelected university teachingweb.mit.eduRead source
    3. 17.2 Combined Conduction and ConvectionMIT Unified Engineering · Thermodynamics and PropulsionSelected university teachingweb.mit.eduRead source
  3. Passive Thermal Control Engineering GuidebookNASA · Revision 5.1, 19 December 2024Selected historical engineering guide sections · PDFntrs.nasa.govRead source