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NASA-TN-D-3149
Influence of programming techniques and of varying limit load factor on maneuver load fatigue test results
Year: 1966
Abstract: Variable amplitude axial load fatigue test on notched aluminum alloy specimens - aircraft component testing.
Subject: AIRCRAFT PART
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:18:05Z | |
| date available | 2017-09-04T15:18:05Z | |
| date copyright | 01/01/1966 | |
| date issued | 1966 | |
| identifier other | MPBBFEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/17644 | |
| description abstract | Variable amplitude axial load fatigue test on notched aluminum alloy specimens - aircraft component testing. | |
| language | English | |
| title | NASA-TN-D-3149 | num |
| title | Influence of programming techniques and of varying limit load factor on maneuver load fatigue test results | en |
| type | standard | |
| page | 17 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1966 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT PART | |
| subject keywords | AIRCRAFT PARTS | |
| subject keywords | ALUMINUM ALLOY | |
| subject keywords | ALUMINUM ALLOYS | |
| subject keywords | AXIAL LOAD | |
| subject keywords | AXIAL LOADS | |
| subject keywords | FATIGUE TEST | |
| subject keywords | FATIGUE TESTS | |
| subject keywords | LOAD TESTS | |
| subject keywords | LOADS (FORCES) | |
| subject keywords | METAL FATIGUE | |
| subject keywords | NOTCH TESTS | |
| subject keywords | NOTCHED METAL |