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Jet engine nozzle exit configurations and associated systems and methods (Document No: 20140016614)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 2013 |
| Description | Nozzle exit configurations and associated systems and methods are disclosed. An aircraft system in accordance with one embodiment includes a jet engine exhaust nozzle having an internal flow surface and an exit aperture, with the exit aperture having a perimeter that includes multiple projections extending in an aft direction. Aft portions of individual neighboring projections are spaced apart from each other by a gap, and a geometric feature of the multiple can change in a monotonic manner along at least a portion of the perimeter. |
| File Size | 1222598 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20140016614 |
| Archival Resource Key | ark:/13960/t0kt1pq0d |
| Language | English |
| Publisher Date | 2013-08-20 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Acoustics Patents Exhaust Nozzles Jet Aircraft Noise Noise Reduction Jet Nozzles Jet Aircraft Apertures Variable Geometry Structures Propulsion System Configurations Aircraft Configurations 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 |
