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Powder metallurgy approaches to high temperature components for gas turbine engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Probst, H. B. |
| Copyright Year | 1974 |
| Description | Research is reported for the tensile strength, ductility, and heat performance characterisitics of powder metallurgy (p/m) superalloys. Oxide dispersion strengthened alloys were also evaluated for their strength during thermal processing. The mechanical attributes evident in both p/m supperalloys and dispersion strengthened alloys are discussed in terms of research into their possible combination. |
| File Size | 688163 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019851 |
| Archival Resource Key | ark:/13960/t4qk26574 |
| Language | English |
| Publisher Date | 1974-01-01 |
| Access Restriction | Open |
| Subject Keyword | Materials, Metallic Refractory Materials Ductility Heat Resistant Alloys Gas Turbine Engines High Temperature Tests Mechanical Properties Powder Metallurgy Thermal Stability Oxide Dispersion Strengthening Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
