NASA-TM-X-3316
An investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steels
Year: 1975
Abstract: The elastic fracture toughness of the three steels is shown to not decrease significantly with decreasing temperature from room temperature to about 244 K (-20 F.). The elastic fracture toughness of the three steels increased with increasing specimen width and thickness. The fatigue-crack-growth data for all three steels fall into relatively narrow scatter bands on plots of rate against stress-intensity range. An equation is shown to predict the upper bounds of the scatter bands reasonably well. Charpy impact energies decreased with decreasing temperature in the nominal temperature range from room temperature to 244 K (-20 F). The nil-ductility temperatures of the steels are discussed.
Subject: CHARPY IMPACT TEST
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:12:47Z | |
| date available | 2017-09-04T15:12:47Z | |
| date copyright | 01/01/1975 | |
| date issued | 1975 | |
| identifier other | LYHOEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/11316 | |
| description abstract | The elastic fracture toughness of the three steels is shown to not decrease significantly with decreasing temperature from room temperature to about 244 K (-20 F.). The elastic fracture toughness of the three steels increased with increasing specimen width and thickness. The fatigue-crack-growth data for all three steels fall into relatively narrow scatter bands on plots of rate against stress-intensity range. An equation is shown to predict the upper bounds of the scatter bands reasonably well. Charpy impact energies decreased with decreasing temperature in the nominal temperature range from room temperature to 244 K (-20 F). The nil-ductility temperatures of the steels are discussed. | |
| language | English | |
| title | NASA-TM-X-3316 | num |
| title | An investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steels | en |
| type | standard | |
| page | 57 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1975 | |
| contenttype | fulltext | |
| subject keywords | CHARPY IMPACT TEST | |
| subject keywords | CRACKING (FRACTURING) | |
| subject keywords | DUCTILITY | |
| subject keywords | FATIGUE (MATERIALS) | |
| subject keywords | FRACTURE STRENGTH | |
| subject keywords | IMPACT LOADS | |
| subject keywords | PRESSURE VESSELS | |
| subject keywords | STEELS | |
| subject keywords | STRESS ANALYSIS | |
| subject keywords | TABLES (DATA) | |
| subject keywords | TEMPERATURE EFFECTS |

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