3. 3
Differences between ideal solution vs. realistic solution
(a) (b) (c)
(a) ideal alignment, (b) non-ideal alignment, (c) line of flux
Stress distribution showing in Figures (d), (e) and (f) in the maxZ plane
σzz
σzy
(e) (f)
σzx
(d)
4. 4
Results for the prediction of Effective Thermal
Expansion Coefficient (αeff)
• Predicted displacements in x, y and z directions.
-6.343e-08 < ux < 6.343e-08
x-direction
-5.0145e-11< uy < 1.2506e-07 -6.43e-08 < ux < 6.43e-08
y-direction z-direction
5. 5
(a) Relation between αeff and P (b) αeff vs. Schapery Upper and lower bounds
Comparison of predicted αeff results with Schapery
upper and lower bounds.
9.84E-06
9.86E-06
9.88E-06
9.9E-06
9.92E-06
9.94E-06
9.96E-06
9.98E-06
0.25 0.3 0.35 0.4 0.45
EffectiveThermalExpansion
Coefficient,αeff(/K)
Porosity, P
0.0E+00
5.0E-06
1.0E-05
1.5E-05
2.0E-05
2.5E-05
3.0E-05
0.25 0.27 0.29 0.31 0.33 0.35 0.37 0.39 0.41
EffectiveThermalExpansion
Coefficient,αeff(/K) Porosity, P
FV solution
Schapery upper bound
Schapery lower bound