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Thrust vector control for v/stol aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Toney, E. W. |
| Copyright Year | 1974 |
| Description | To deflect exhaust of V/STOL aircraft fan deploy set of rectangular flaps so exhaust stream can be turned as required and then directed through exit nozzles which generate thrust in appropriate direction; lateral deflection of exhaust is provided by yaw vanes. |
| File Size | 88786 |
| Page Count | 2 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740000049 |
| Archival Resource Key | ark:/13960/t6m08w85t |
| Language | English |
| Publisher Date | 1974-05-01 |
| Access Restriction | Open |
| Subject Keyword | V/stol Aircraft Exhaust Nozzles Jet Flow Thrust Vector Control Flaps Control Surfaces Aircraft Launching Devices Aircraft Control Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |