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Turbine blade thermal fatigue testing pratt and whitney aircraft hollow core blades
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gross, L. Ingram, J. |
| Copyright Year | 1985 |
| Description | The results of low cycle fatigue testing on turbine blades for use in hydrogen/oxygen rocket engines is presented. Cored blade and cored blades with circulation were tested in the MSFC thermal fatigue tester. Both blade configurations showed significant low cycle fatigue life improvements when compared to baseline solid blades. |
| File Size | 1423421 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860004801 |
| Archival Resource Key | ark:/13960/t94798j76 |
| Language | English |
| Publisher Date | 1985-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Fatigue Tests Turbomachine Blades Metal Fatigue Fatigue Life Failure Analysis Fatigue Materials Turbine Wheels Thermal Cycling Tests Turborocket Engines Hydrogen Oxygen Engines 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 |