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Determination of design allowable properties. fracture of 2219-t87 aluminum alloy
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Engstrom, W. L. |
| Copyright Year | 1972 |
| Description | A literature survey was conducted to provide a comprehensive report of available valid data on tensile properties, fracture toughness, fatigue crack propagation, and sustained load behavior of 2219-T87 aluminum alloy base metal and weldments, as applicable to manned spacecraft tankage. Most of the data found were from tests conducted at room temperature, -320 F and -423 F. Data are presented in graphical and tabular form, and areas in which data are lacking are established. |
| File Size | 11948772 |
| Page Count | 252 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720025881 |
| Archival Resource Key | ark:/13960/t1hj1909p |
| Language | English |
| Publisher Date | 1972-03-01 |
| Access Restriction | Open |
| Subject Keyword | Materials, Metallic Welding Fatigue Materials Aluminum Alloys Fracture Strength Tensile Properties Loads Forces Crack Propagation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
