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1 - Erich Schmid Institute

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E.4 Calculation of the Normal Stresses in the Substrate and the Coating<br />

Figure E.3: Axial forces or the corresponding bending moments, respectively, establish the equilibrium<br />

of the system, compensate for the difference in length and straighten the system.<br />

E.4 Calculation of the Normal Stresses in the Substrate and<br />

the Coating<br />

The force F = −F1 = F2 compensates for the difference in length of the layer and the<br />

substrate. Calculation of the strains ɛ1 and ɛ2 owing to thermal expansion ∆T :<br />

ɛ1 = ∆l1<br />

l = α1∆T (E.9)<br />

ɛ2 = ∆l2<br />

l = α2∆T (E.10)<br />

Calculation of the strains ɛ1F and ɛ2F owing to to the applied forces F1 and F2:<br />

ɛ1F = σ1<br />

E1<br />

ɛ2F = σ2<br />

E2<br />

σ1 = F1<br />

A1<br />

σ2 = F2<br />

A2<br />

A1 = bt1<br />

A2 = bt2<br />

= ∆l1F<br />

l + ∆l1<br />

= ∆l2F<br />

l + ∆l2<br />

= − F<br />

A1<br />

= F<br />

A2<br />

= − F<br />

t1b<br />

= F<br />

t2b<br />

(E.11)<br />

(E.12)<br />

(E.13)<br />

(E.14)<br />

(E.15)<br />

(E.16)<br />

Calculation of the lengths l1 and l2 of the coating and the substrate subjected to ∆T :<br />

l1 = l + ∆l1 = l + ɛ1 · l = l (1 + ɛ1) (E.17)<br />

l2 = l + ∆l2 = l + ɛ2 · l = l (1 + ɛ2) (E.18)<br />

Now the difference in length is compensated by applying F1 and F2 which leads to the<br />

strains ɛ1F and ɛ2F .<br />

E–5<br />

E

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