| 000 | 00769pam a2200217a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
| 245 | 1 |
_aNASA Technical Note [NASA TN D-543]: Fatigue-crack propagation in aluminum-alloy tension panels _cRichard E. Whaley and Peter R. Kurzhals |
|
| 260 |
_bNASA _c1960 _aWashington |
||
| 300 | _a25p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-541 to 550 | ||
| 500 | _aBound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862 | ||
| 650 | _aStresses and loades | ||
| 700 | _aWhaley, Richard E. | ||
| 700 | _aKurzhals, Peter R. | ||
| 942 | _cBK | ||
| 999 |
_c399459 _d399459 |
||