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Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carson Jr., George T. Capone, Francis J. |
| Copyright Year | 1991 |
| Description | An investigation was conducted in the static test facility of the Langley 16 Foot Transonic Tunnel in order to determine the internal performance characteristics of a multiaxis thrust vectoring axisymmetric nozzle. Thrust vectoring for this nozzle was achieved by deflection of only the divergent section of this nozzle. The effects of nozzle power setting and divergent flap length were studied at nozzle deflection angles of 0 to 30 at nozzle pressure ratios up to 8.0. |
| File Size | 3268505 |
| Page Count | 82 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910005812 |
| Archival Resource Key | ark:/13960/t0ns5nw5f |
| Language | English |
| Publisher Date | 1991-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Test Facilities Nozzle Design Deflection Transonic Wind Tunnels Thrust Vector Control Wind Tunnel Tests Convergent-divergent Nozzles Pressure Ratio Static Tests Flapping Axisymmetric Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |