Table 6.
Stress type | Stress part | ||||||
---|---|---|---|---|---|---|---|
1st principal stress | 0.536 | 0.438 | 0.248 | 0.343 | 0.506 | 0.522 | |
2nd principal stress | 0.415 | 0.290 | 0.323 | 0.320 | 0.495 | 0.419 | |
3rd principal stress | 0.041 | 0.089 | 0.192 | 0.178 | 0.170 | 0.186 | |
fiber stress | 0.522 | 0.410 | 0.252 | 0.366 | 0.492 | 0.517 | |
Stress magnitude | 0.578 | 0.480 | 0.266 | 0.370 | 0.547 | 0.574 | |
Von Mises stress | 0.552 | 0.448 | 0.207 | 0.290 | 0.483 | 0.484 | |
1st principal stress | 0.536 | 0.310 | 0.248 | 0.307 | 0.506 | 0.424 | |
2nd principal stress | 0.415 | 0.288 | 0.323 | 0.251 | 0.495 | 0.352 | |
3rd principal stress | 0.041 | 0.273 | 0.192 | 0.266 | 0.170 | 0.378 | |
Fiber stress | 0.522 | 0.402 | 0.252 | 0.299 | 0.492 | 0.471 | |
Stress magnitude | 0.578 | − 0.244 | 0.266 | − 0.206 | 0.547 | − 0.322 | |
Von Mises stress | 0.552 | 0.126 | 0.207 | 0.135 | 0.483 | 0.171 | |
1st principal stress | – | 0.222 | – | 0.172 | – | 0.259 | |
2nd principal stress | – | 0.086 | – | 0.063 | – | 0.077 | |
3rd principal stress | – | − 0.096 | – | − 0.034 | – | 0.067 | |
Fiber stress | – | 0.214 | – | 0.269 | – | 0.314 | |
Stress magnitude | – | 0.401 | – | 0.317 | – | 0.462 | |
Von Mises stress | – | 0.285 | – | 0.206 | – | 0.318 | |
1st principal stress | 0.553 | 0.374 | 0.249 | 0.333 | 0.517 | 0.483 | |
2nd principal stress | 0.388 | 0.315 | 0.308 | 0.280 | 0.469 | 0.399 | |
3rd principal stress | 0.041 | 0.145 | 0.149 | 0.266 | 0.133 | 0.289 | |
Fiber stress | 0.532 | 0.390 | 0.272 | 0.358 | 0.515 | 0.504 | |
Stress magnitude | 0.595 | 0.456 | 0.282 | 0.393 | 0.569 | 0.578 | |
Von Mises stress | 0.576 | 0.375 | 0.174 | 0.185 | 0.474 | 0.365 |
Shown is total Cauchy stress (), passive Cauchy stress (), active Cauchy stress (), and total second Piola-Kirchhoff stress (). For each the stress magnitude, first, second, and third principal stress, fiber stress, and von Mises stress is computed. Spearman- values for correlation: inverse of wall thickness (), inverse of curvature (), inverse of (thickness curvature) () each versus stress at inflation () and contraction (). Active stress is 0 at the point of inflation, hence, results are omitted