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Advanced blade tip seal system, volume 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zelahy, J. W. Fairbanks, N. P. |
| Copyright Year | 1982 |
| Description | The results of the endurance and performance engine tests conducted on monocrystal/abrasive-tipped CF6-50 Stage 1 HPT blades fabricated in Task VII of MATE Project 3 are presented. Two engine tests are conducted. The endurance engine test is conducted for 1000 C cycles. The performance engine test is conducted on a variable cycle core engine. Posttest evaluation and analyses of the blades and shrouds included visual, dimensional, and destructive evaluations. |
| File Size | 9983552 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850002691 |
| Archival Resource Key | ark:/13960/t1zd2rj5b |
| Language | English |
| Publisher Date | 1982-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Blade Tips Performance Tests Fracture Mechanics Composite Materials Rotor Blades Turbomachinery Inspection Turbomachinery Engine Tests Crack Initiation 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 |
