| 000 | 00599 a2200241 4500 | ||
|---|---|---|---|
| 001 | 338115 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TN D 6376 : 1971 | ||
| 245 | _aImproved method of collocation for the stress analysis of cracked plates with various shaped boundaries | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNASA | ||
| 260 | _c1971 | ||
| 300 | _a45 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TN D 6376 : 1971 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aCollocation, Cracks, Stress-intensity factors, Stress analysis, Numerical analysis | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c205164 _d205164 |
||