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CONSTITUTIVE EQUATIONS FOR SOLID PROPELLANTS

CONSTITUTIVE EQUATIONS FOR SOLID PROPELLANTS

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1<br />

0.8<br />

Stress (MPa)<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

10%<br />

20%<br />

monotonic<br />

0 0.1 0.2 0.3 0.4<br />

Strain<br />

0.12<br />

0.09<br />

Dilatation<br />

0.06<br />

0.03<br />

10%<br />

20%<br />

monotonic<br />

0.00<br />

0 0.1 0.2 0.3 0.4<br />

Strain<br />

Figure 2<br />

(Sebnem Ozupek)<br />

24

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