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Retardation analytical model to extend service life (Document No: 19840024791)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Matejczyk, D. |
| Copyright Year | 1984 |
| Description | A fatigue crack growth model that incorporates crack growth retardation effects and is applicable to the materials characteristics and service environments of high performance LH2/LO2 engine systems was developed and tested. |
| File Size | 212784 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840024791 |
| Archival Resource Key | ark:/13960/t51g5j432 |
| Language | English |
| Publisher Date | 1984-09-08 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Performance Tests Stellite Trademark Fatigue Materials Mathematical Models Hydrogen Oxygen Engines Crack Arrest Tensile Strength Inconel Trademark Loads Forces Crack Propagation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |