| 000 | 01824nam a2200409Ia 4500 | ||
|---|---|---|---|
| 001 | 270472 | ||
| 003 | OCoLC | ||
| 005 | 20160527194238.0 | ||
| 007 | he bmb024bbca | ||
| 008 | 040716s2003 vaua bb f000 0 eng d | ||
| 040 |
_aGPO _cGPO |
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| 049 | _aPUXA | ||
| 074 | _a0830-D (MF) | ||
| 074 | _a0830-D (online) | ||
| 086 | 0 | _aNAS 1.15:212166 | |
| 100 | 1 |
_aSmith, Stephen W. _2Local _9171508 |
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| 245 | 1 | 0 |
_aSimulation of fatigue crack initiation at corrosion pits with EDM notches _h[microform] _cStephen W. Smith, John A. Newman, [and] Robert S. Piascik. |
| 260 |
_aHampton, Va. _bNational Aeronautics and Space Administration, Langley Research Center _aHanover MD _bAvailable from NASA Center for AeroSpace Information (CASI) _c[2003] |
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| 300 | _a1 v. | ||
| 490 | 1 |
_aNASA/TM _v2003-212166 _2Local _9140973 |
|
| 500 | _aShipping list no.: 2004-0306-M. | ||
| 500 | _a"March 2003." | ||
| 530 | _aAlso available via Internet from the NASA Web site. Address as of 7/14/04: http://techreports.larc.nasa.gov/ltrs/PDF/2003/tm/NASA-2003-tm212166.pdf; current access available via PURL. | ||
| 504 | _aIncludes bibliographical references. | ||
| 533 |
_aMicrofiche. _b[Washington, D.C.] _cSupt. of Docs., U.S. G.P.O. _d[2003]. _e1 microfiche : negative. |
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| 650 | 7 |
_aFatigue tests. _2nasat _2Local _994902 |
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| 650 | 7 |
_aAluminum alloys. _2nasat _2Local _951522 |
|
| 650 | 7 |
_aStress corrosion. _2nasat _2Local _9175067 |
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| 650 | 7 |
_aCorrosion. _2nasat _2Local _981077 |
|
| 650 | 7 |
_aCrack initiation. _2nasat _2Local _981748 |
|
| 650 | 7 |
_aSimulation. _2nasat _2Local _9170613 |
|
| 700 | 1 |
_aNewman, John A. _2Local _9142516 |
|
| 700 | 1 |
_aPiascik, Robert S. _2Local _9150908 |
|
| 710 | 2 |
_aLangley Research Center _2Local _9122979 |
|
| 830 | 0 |
_aNASA technical memorandum _v211266. |
|
| 856 | 4 | 1 | _uhttp://purl.access.gpo.gov/GPO/LPS51481 |
| 999 |
_c195297 _d195297 |
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