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Aircraft engine nozzle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sorensen, N. E. |
| Copyright Year | 1980 |
| Description | A variable area exit nozzle arrangement for an aircraft engine was a substantially reduced length and weight which comprises a number of longitudinally movable radial vanes and a number of fixed radial vanes. The movable radial vanes are alternately disposed with respect to the fixed radial vanes. A means is provided for displacing the movable vanes along the longitudinal axis of the engine relative to the fixed radial vanes which extend across the main exhaust flow of the engine. |
| File Size | 477351 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800023884 |
| Archival Resource Key | ark:/13960/t04z03m3f |
| Language | English |
| Publisher Date | 1980-07-29 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Nozzle Design Length Supersonic Nozzles Jet Aircraft Weight Reduction Convergent-divergent Nozzles Aircraft Engines Variable Geometry Structures Jet Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
