This page is a drill sheet. The parent topic gave you four formulas; here we push them into every corner — the safe case, the failure case, the degenerate case (zero jump, zero conductivity), the limiting case (huge stiffness), a word problem, and an exam twist. Before we compute anything, let us agree on what every symbol means, so a reader who has never seen them can follow line one.
Definition The five symbols we will keep reusing
Δ T = temperature jump in kelvin (K). "How many degrees hotter one face suddenly got than the interior." A jump of 200 K means 200 degrees difference — same size in °C or K, since only the difference matters.
α = linear thermal expansion coefficient , units 1/ K . "Fractional length gained per degree." If α = 8 × 1 0 − 6 / K , then heating 1 metre by 1 K lengthens it by 8 micrometres.
E = Young's modulus (stiffness), units Pa. "How hard the material fights being stretched." Big E = very stiff, so a tiny forced strain becomes a huge stress.
ν = Poisson's ratio (dimensionless, ~0.2 for ceramics). It appears as ( 1 − ν ) because a hot surface is squeezed in two directions at once (biaxial), not one.
σ f = fracture strength in Pa. "The stress at which a crack runs and the part breaks."
Intuition Why these tools and not others?
We use Hooke's law (σ = E ε ) because a restrained thermal strain has nowhere to go — it converts directly into stress. We use Fourier's law (q = k Δ T / L ) for coatings because we want to know how much heat leaks through a thin insulating skin. And R is just algebra: "at what jump does the built stress equal the breaking stress?"
Every question this topic can ask is one of these cells:
Cell
What it tests
Degenerate/limit knob
Example
A. Safe shock
σ t h < σ f → survives
—
Ex 1
B. Failing shock
σ t h > σ f → cracks
—
Ex 2
C. Zero jump
Δ T = 0
σ t h → 0
Ex 3
D. Rank materials
compare R across the four ceramics
which wins & why
Ex 4
E. Free expansion
tolerance from Δ L
—
Ex 5
F. Coating heat block
Fourier q , low-k payoff
k → small
Ex 6
G. Limiting stiffness
E → huge / ν → 0.5
asymptotic R
Ex 7
H. Word problem
pick the right ceramic for a duty
—
Ex 8
I. Exam twist
transformation toughening K I c
crack-tip case
Ex 9
The examples below hit every cell.
Worked example (1) CELL A — Does silicon nitride survive a 500 K shock?
Data: σ f = 800 MPa, E = 310 GPa, α = 3.0 × 1 0 − 6 / K , ν = 0.27 , Δ T = 500 K.
Forecast: Si₃N₄ is famous for shock resistance — I bet the induced stress stays below 800 MPa. Guess before reading on.
Compute the induced stress.
σ t h = 1 − ν E α Δ T = 1 − 0.27 310 × 1 0 9 ⋅ 3.0 × 1 0 − 6 ⋅ 500 .
Why this step? The cold interior restrains the hot face; that forbidden strain α Δ T becomes stress through Hooke's law, boosted by 1/ ( 1 − ν ) for biaxial squeeze.
Numerator = 310 × 1 0 9 ⋅ 1.5 × 1 0 − 3 = 4.65 × 1 0 8 . Divide by 0.73 : σ t h ≈ 6.37 × 1 0 8 Pa = 637 MPa.
Compare to fracture strength. 637 < 800 MPa → survives.
Why this step? A crack only runs once stress reaches σ f ; we are safely under it.
Verify: Independently, R = E α σ f ( 1 − ν ) = 310 × 1 0 9 ⋅ 3.0 × 1 0 − 6 800 × 1 0 6 ⋅ 0.73 ≈ 628 K. Our jump 500 K < 628 K, consistent with "survives." Units: Pa·(–)/[Pa·(1/K)] = K. ✓
Worked example (2) CELL B — Same shock on alumina: it cracks.
Data: σ f = 300 MPa, E = 380 GPa, α = 8.0 × 1 0 − 6 / K , ν = 0.22 , Δ T = 500 K.
Forecast: alumina has weaker strength and bigger α than Si₃N₄. Both push toward failure. Predict: cracks.
Induced stress. σ t h = 0.78 380 × 1 0 9 ⋅ 8.0 × 1 0 − 6 ⋅ 500 .
Why this step? Same physics as Ex 1 — build the constrained stress.
Numerator = 380 × 1 0 9 ⋅ 4.0 × 1 0 − 3 = 1.52 × 1 0 9 . Divide by 0.78 : σ t h ≈ 1.95 × 1 0 9 Pa = 1949 MPa.
Compare. 1949 ≫ 300 MPa → cracks catastrophically.
Why: stress is over 6× the breaking stress; a crack runs instantly.
Verify: Safe limit R = 380 × 1 0 9 ⋅ 8.0 × 1 0 − 6 300 × 1 0 6 ⋅ 0.78 ≈ 77 K. The actual 500 K jump dwarfs 77 K — alumina is hopeless for this duty, matching the parent note's "~77 K" result. ✓
Worked example (3) CELL C — The degenerate case: zero temperature jump.
Data: any ceramic, but Δ T = 0 K.
Forecast: No jump, no fight — stress should be exactly zero. This is the sanity-check cell every formula must pass.
Plug in. σ t h = 1 − ν E α ⋅ 0 = 0 Pa.
Why this step? Thermal stress comes only from a restrained temperature difference. Uniform temperature = every atom expands the same = no atom is forced against a neighbour = zero stress.
Interpretation. A part heated slowly and uniformly (interior and surface at the same T ) develops no thermal stress , even at 1500 °C. Thermal shock is about the gradient , not the absolute temperature.
Why: this is why a furnace ramp is gentle and a quench is lethal.
Verify: σ t h ( 0 ) = 0 trivially; and R for Δ T = 0 is undefined as a jump but the survivable margin is infinite — you can hold zero-gradient parts forever. ✓
Worked example (4) CELL D — Rank all four ceramics by shock resistance
R .
Data (approx):
Ceramic
σ f /MPa
E /GPa
α /(1 0 − 6 K− 1 )
ν
Alumina
300
380
8.0
0.22
Zirconia (PSZ)
600
200
10.0
0.30
SiC
400
410
4.5
0.17
Si₃N₄
800
310
3.0
0.27
Forecast: R = σ f ( 1 − ν ) / ( E α ) rewards high strength, low stiffness, low expansion . Si₃N₄ has tiny α and high σ f → I predict it wins; alumina loses.
Compute each R (units K).
Alumina: 380 ⋅ 8.0 300 ⋅ 0.78 × 1 0 9 ⋅ 1 0 − 6 1 0 6 = 3040 234 × 1 0 3 ≈ 77 K.
Zirconia: 200 ⋅ 10.0 600 ⋅ 0.70 × 1 0 3 = 2000 420 × 1 0 3 = 210 K.
SiC: 410 ⋅ 4.5 400 ⋅ 0.83 × 1 0 3 = 1845 332 × 1 0 3 ≈ 180 K.
Si₃N₄: 310 ⋅ 3.0 800 ⋅ 0.73 × 1 0 3 = 930 584 × 1 0 3 ≈ 628 K.
Why this step? Direct application of the figure-of-merit; the 1 0 6 / ( 1 0 9 ⋅ 1 0 − 6 ) = 1 0 3 factor keeps units in K.
Rank: Si₃N₄ (628) > Zirconia (210) > SiC (180) > Alumina (77).
Why: Si₃N₄'s tiny α = 3 × 1 0 − 6 is the dominant reason — expansion sits in the denominator. See figure.
Verify: All four numbers rechecked below; ordering Si₃N₄ > ZrO₂ > SiC > Al₂O₃ confirmed. This matches the parent's claim that Si₃N₄ has the "best thermal-shock resistance." ✓
Worked example (5) CELL E — Free thermal growth of a SiC part (tolerance check).
A 50 mm SiC guide vane goes from 25 ∘ C to 1225 ∘ C . α = 4.5 × 1 0 − 6 / K .
Forecast: SiC barely expands. On 50 mm over 1200 K, I expect a fraction of a millimetre.
Temperature jump. Δ T = 1225 − 25 = 1200 K.
Why this step? Expansion depends on the difference , and a difference of 1200 °C equals 1200 K.
Length change. Δ L = α L 0 Δ T = ( 4.5 × 1 0 − 6 ) ( 0.050 ) ( 1200 ) .
Why: with α roughly constant, growth is just α integrated over the jump = α L 0 Δ T . No restraint here, so no stress — the part is free to grow.
= 4.5 × 1 0 − 6 ⋅ 60 = 2.7 × 1 0 − 4 m = 0.27 mm.
Verify: 0.27 mm on 50 mm is 0.54% — tiny, so precision fits survive hot. Matches parent Ex 2. Units: ( 1/ K ) ( m ) ( K ) = m . ✓
Worked example (6) CELL F — Heat blocked by a zirconia thermal-barrier coating.
A 0.3 mm zirconia TBC (see Thermal Barrier Coatings on Superalloys ): outer face 1200 ∘ C , metal side 950 ∘ C , k = 2 W/m·K.
Forecast: Thin layer but very low k . I expect a heat flux of order a million W/m².
Jump across the coating. Δ T = 1200 − 950 = 250 K.
Why this step? Fourier's law uses the temperature drop over the layer, and 250 °C = 250 K.
Flux. q = k L Δ T = 2 ⋅ 3 × 1 0 − 4 250 .
Why: heat flows down the gradient; a thin L with small k still passes some heat, and we quantify it.
= 2 ⋅ 8.33 × 1 0 5 = 1.67 × 1 0 6 W/m².
Payoff vs alumina. Same geometry with k = 30 gives q = 30 ⋅ 250/3 × 1 0 − 4 = 2.5 × 1 0 7 W/m² — 15× more heat .
Why: the entire reason zirconia coats blades is its low k ; alumina would dump too much heat into the metal.
Verify: 1.67 × 1 0 6 W/m² (matches parent Ex 3); ratio 30/2 = 15 confirms the 15× claim. Units: (W/m·K)(K)/(m) = W/m². ✓
Worked example (7) CELL G — Limiting behaviour: what if the material were infinitely stiff, or
ν → 0.5 ?
Forecast: Both E and ( 1 − ν ) live in R . Very large E should drive R → 0 ; ν → 0.5 (incompressible) should also shrink R .
Stiffness limit. R = E α σ f ( 1 − ν ) ; as E → ∞ , R → 0 .
Why this step? An infinitely stiff bond turns even a microscopic restrained strain into infinite stress — the part shatters at the tiniest gradient. This is why very stiff ceramics (SiC, alumina) are shock-prone despite being "strong."
Poisson limit. As ν → 0.5 , ( 1 − ν ) → 0.5 , halving R relative to ν → 0 .
Why: higher ν means the biaxial squeeze is fiercer, raising σ t h and lowering the survivable jump.
Numeric feel: take Si₃N₄ but pretend E doubled to 620 GPa. R = 620 × 1 0 9 ⋅ 3.0 × 1 0 − 6 800 × 1 0 6 ⋅ 0.73 ≈ 314 K — exactly half of 628 K.
Why: R ∝ 1/ E , so doubling E halves R . This isolates stiffness as the villain.
Verify: 314 K = 628/2 within rounding confirms the 1/ E scaling. ✓
Worked example (8) CELL H — Word problem: choose a ceramic for a rocket nozzle throat.
Requirement: survives repeated ≈ 400 K quench cycles, sits in oxygen-rich combustion, must not peel, keep tight shape.
Forecast: "Oxygen-rich" hints at an oxide (won't burn). "Survive 400 K quench" needs R ≳ 400 K. Let me see which oxide qualifies.
Screen by oxidation. Oxidising atmosphere → favour oxides (Al₂O₃, ZrO₂); non-oxides SiC/Si₃N₄ can work via their protective SiO₂ skin but risk active oxidation if O₂ is low — here O₂ is plentiful, so passive skin is fine too. Keep all four as candidates.
Why this step? Chemistry gates the shortlist before mechanics does.
Screen by shock R ≥ 400 K (from Ex 4): only Si₃N₄ (628 K) clears 400 K comfortably; zirconia (210) and SiC (180) and alumina (77) fail the repeated-quench bar.
Why: the cycling stress must stay below σ f every cycle.
Decision: pick Si₃N₄ . Its high σ f and tiny α give margin; its SiO₂ passive layer handles the O₂-rich gas up to ~1600 °C.
Why: it is the only candidate meeting both chemistry and shock — the classic reason Si₃N₄ is chosen for the harshest thermal-cycling parts.
Verify: R Si 3 N 4 = 628 K > 400 K margin factor 1.57 ; all others < 400 K, so the choice is forced. ✓
Worked example (9) CELL I — Exam twist: fracture toughness of transformation-toughened zirconia.
The matrix toughness is K I c matrix = 3.2 MPa⋅m 1/2 ; transformation toughening at the crack tip adds Δ K = 6.3 MPa⋅m 1/2 (see Phase Transformations and Thermal Stress and Fracture Mechanics ).
Forecast: The tetragonal→monoclinic + 4% volume jump slams the crack shut. I expect total K I c near the 8 –12 range the parent quotes.
Add the contributions. K I c tough = K I c matrix + Δ K = 3.2 + 6.3 = 9.5 MPa⋅m 1/2 .
Why this step? The extra work the crack must do to force the local transformation adds to the intrinsic resistance — a superposition of the crack-tip shielding.
Compare to alumina (K I c ≈ 4 ): ratio 9.5/4 ≈ 2.4 → zirconia is ~2.4× tougher.
Why: explains why zirconia — despite modest σ f — is the "toughest ceramic": the crack tries to open a door, the crystal slams a bigger one shut.
Verify: 3.2 + 6.3 = 9.5 lands inside the quoted 8 –12 MPa·m1/2 band; ratio to alumina ≈ 2.4 . ✓
Recall Quick self-test
Why does zero temperature jump give zero thermal stress? ::: Stress needs a restrained gradient ; if all atoms expand equally there is nothing to fight, so σ t h = E α ⋅ 0/ ( 1 − ν ) = 0 .
In R = σ f ( 1 − ν ) / ( E α ) , which single property makes Si₃N₄ win? ::: Its tiny α ≈ 3 × 1 0 − 6 / K sitting in the denominator.
A stiffer ceramic (bigger E ) is more or less shock-resistant? ::: Less — R ∝ 1/ E , so stiffness lowers the survivable jump.
Mnemonic The shock cheat-code
"Weak-and-still": you WANT weak stiffness (E ↓), strong break (σ f ↑), and still dimensions (α ↓). All three point the same way in R .
Related deep material: Ceramic Matrix Composites (CMCs) , Nickel Superalloys , Crystal Bonding — Ionic vs Covalent .