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Abradable compressor and turbine seals, volume 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sundberg, D. V. Hurst, L. G. Dennis, R. E. |
| Copyright Year | 1979 |
| Description | The applications and advantages of abradable coatings as gas path seals in a general aviation turbofan engine were investigated. Abradable materials were evaluated for the high pressure radial compressor and the axial high and low pressure turbine shrouds. |
| File Size | 4396048 |
| Page Count | 74 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810018560 |
| Archival Resource Key | ark:/13960/t8jd9p67v |
| Language | English |
| Publisher Date | 1979-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Shrouded Turbines Sealers Abrasion Seals Stoppers Axial Flow Turbines Turbofan Engines Engine Tests Aircraft Engines Coatings Engine Parts 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 |