| 000 | 00625 a2200241 4500 | ||
|---|---|---|---|
| 001 | 357866 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TN D-6899 : 1972 | ||
| 245 | _aFatigue crack growth from a circular hole with and without high prior loading | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautcs ad space Association | ||
| 260 | _c1972 | ||
| 300 | _a33 P. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TN D-6899 : 1972 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aCrack propagation,Stress concentration,Stress intensity factors,High prior loading,Residual stress | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c229663 _d229663 |
||