| 000 | 00614pam a2200181a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aHudson, C. Michael | ||
| 245 | 1 |
_aEFFECT OF STRESS RATIO ON FATIGUE-CRACK GROWTH IN 7075-T-6 AND 2024-T-3 ALUMINUM-ALLOY SPECIMENS [NASA TN D-5390] _cHudson, Michael C. |
|
| 260 |
_bNational Aeronautics and Space Administration _c1969 _aWashington, D.C. |
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| 300 | _a29p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNasa Technical Note | ||
| 500 | _aBound vol. contains NASA TN D 5381-5390 | ||
| 650 | _aStress ratio | ||
| 942 | _cTR | ||
| 999 |
_c398464 _d398464 |
||