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Creep-rupture behavior of candidate stirling engine iron supperalloys in high-pressure hydrogen. volume 2: hydrogen creep-rupture behavior
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Peterman, W. Hales, C. Bhattacharyya, S. |
| Copyright Year | 1984 |
| Description | The creep rupture behavior of nine iron base and one cobalt base candidate Stirling engine alloys is evaluated. Rupture life, minimum creep rate, and time to 1% strain data are analyzed. The 3500 h rupture life stress and stress to obtain 1% strain in 3500 h are also estimated. |
| File Size | 33635419 |
| Page Count | 114 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840020892 |
| Archival Resource Key | ark:/13960/t6zw6935v |
| Language | English |
| Publisher Date | 1984-06-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Service Life Annealing Creep Properties Stress Analysis Fracture Mechanics Hydrogen Iron Alloys Piston Engines High Pressure Stirling Cycle Problem Solving Rupturing Stirling Engines Fractography Cobalt Alloys 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 |
