Loading...
Please wait, while we are loading the content...
Similar Documents
Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Green, Robert S. Carson Jr., George T. |
| Copyright Year | 1987 |
| Description | An investigation was conducted in the Langley 16-Foot Transonic Tunnel at static conditions to measure the pressure distributions inside a nonaxisymmetric nozzle with simultaneous partial thrust reversing (50-percent deployment) and thrust vectoring of the primary (forward-thrust) nozzle flow. Geometric forward-thrust-vector angles of 0 and 15 deg. were tested. Test data were obtained at static conditions while nozzle pressure ratio was varied from 2.0 to 4.0. Results indicate that, unlike the 0 deg. vector angle nozzle, a complicated, asymmetric exhaust flow pattern exists in the primary-flow exhaust duct of the 15 deg. vectored nozzle. |
| File Size | 11239682 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870008239 |
| Archival Resource Key | ark:/13960/t17m55j9x |
| Language | English |
| Publisher Date | 1987-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Nozzle Geometry Exhaust Nozzles Exhaust Gases Transonic Wind Tunnels Thrust Vector Control Wind Tunnel Tests Pressure Distribution Thrust Reversal Static Tests Axisymmetric Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
