| 000 | 00546 a2200265 4500 | ||
|---|---|---|---|
| 001 | 11942 | ||
| 020 | _a0 | ||
| 041 | _aeng | ||
| 080 | _a621.73:620.172.24 Wal | ||
| 245 | _aCrack propagation and residual static strength of typical aircraft forgings | ||
| 250 | _a | ||
| 260 | _aCleveland | ||
| 260 | _bNASA, | ||
| 260 | _c1977 | ||
| 300 | _avarious p. | ||
| 300 | _c27 cm | ||
| 490 | _a | ||
| 100 | _aWalter, Schutz | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aForging | ||
| 650 | _aResidual Stresses | ||
| 942 | _cBK | ||
| 942 | _2UDC | ||
| 999 |
_c13885 _d13885 |
||