درباره ما
NASA-LLIS-0764
Lessons Learned - Controlling Stress Corrosion Cracking in Aerospace Applications
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:26:54Z | |
| date available | 2017-09-04T15:26:54Z | |
| date copyright | 04/06/2000 | |
| date issued | 2000 | |
| identifier other | NPVFQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/27795 | |
| description abstract | Practice: This practice presents considerations that should be evaluated and applied concerning stress corrosion and subsequent crack propagation in mechanical devices, structural devices, and related components used in aerospace applications. Material selection, heat treat methods, fabrication methodology, testing regimes, and loading path assessments are presented as methods to reduce the potential for stress corrosion cracking in a material's operational environment. | |
| language | English | |
| title | NASA-LLIS-0764 | num |
| title | Lessons Learned - Controlling Stress Corrosion Cracking in Aerospace Applications | en |
| type | standard | |
| page | 5 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |
