Table 3.
| Young’s modulus (MPa) | Ultimate strength (MPa) | Ultimate strain (%) | Reference | ||||
|---|---|---|---|---|---|---|---|
| Circumferential | Radial | Circumferential | Radial | Circumferential | Radial | ||
| Pulmonary | 16.05 ± 2.02* | 1.32 ± 0.93* | 2.78 ± 1.05 | 0.29 ± 0.06 | 19.40 ± 3.91 | 29.67 ± 4.41 | [81] |
| Aortic | 15.34 ± 3.84* | 1.98 ± 0.15* | 1.74 ± 0.29 | 0.32 ± 0.04 | 18.35 ± 7.61 | 23.92 ± 3.94 | [81] |
| P > 0.2 | P = 0.002 | P = 0.049 | P > 0.2 | P > 0.2 | P = 0.043 | ||
| Aortic | 15.6 ± 6.4** | 2.0 ± 1.5** | 2.6 ± 1.2 | 0.42 ± 0.24 | 21.9 ± 10.6 | 29.8 ± 13.9 | [103] |
| Aortic | 14.55 ± 3.7*** | 1.57 ± 0.18*** | [104] | ||||
| Porcine aortic | 7.78 ± 1.7*** | 1.28 ± 0.34*** | [104] | ||||
| Porcine aortic | 42.30 ± 4.96* | 5.33 ± 0.61* | 1.58 ± 0.26 | 0.55 ± 0.11 | 7.26 ± 0.69 | 8.57 ± 0.80 | [107] |
Calculated at specimen stress level of 1.0 MPa.
Calculated as the slope of the linear part of the stress-strain curve.
Calculated as the slope a fitted line through the portion of the stress-strain curve between stress levels of 0.4-1.0 MPa for circumferential specimens and 0.05-0.1 MPa for radial specimens.