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Static performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Capone, F. J. |
| Copyright Year | 1978 |
| Description | Transonic tunnel test was performed to determine the static performance of five twin-engine nonaxisymmetric nozzles and a base-line axisymmetric nozzle at three nozzle power settings. Static thrust-vectoring and thrust-reversing performance were also determined. Nonaxisymmetric-nozzle concepts included two-dimensional convergent-divergent nozzles, wedge nozzles, and a nozzle with a single external-expansion ramp. All nonaxisymmetric nozzles had essentially the same statis performance as the axisymmetric nozzle. Effective thrust vectoring and reversing was also achieved. |
| File Size | 3912345 |
| Page Count | 67 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780020114 |
| Archival Resource Key | ark:/13960/t86h9c437 |
| Language | English |
| Publisher Date | 1978-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Nozzle Geometry Static Aerodynamic Characteristics Ramps Structures Thrust Vector Control Convergent-divergent Nozzles Nozzle Thrust Coefficients Thrust Reversal Nozzle Efficiency Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
