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Fluidic Thrust Vectoring Methods
Fluidic thrust vectoring uses small variations in flow created by fluidic devices at different locations in the exhaust flow to produce large responses in the main exhaust stream, resulting in thrust vectoring (Chalmers,1999).
Research into fluidic thrust vectoring has clearly shown the application of flow-control technology to be an effective means of producing vectored thrust.
The application of flow control technology offers many advantages to aircraft thrust vectoring systems. Firstly, fluidic devices have no moving parts interacting with the primary flow. The elimination of moving parts means weight is reduced and reliability is increased. In addition, thrust vectoring with a fixed nozzle geometry allows for the aircraft exhaust section to be shaped for reduced drag, reduced radar signature and to be designed for high temperature conditions (Kowal, 2002). '
http://www.scribd.com/doc/20400973/Thrust-Vectoring
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http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030062131_2003071073.pdf
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Computational fluid dynamics (CFD) was used to simulate the nozzle at typical nozzle pressure ratio (NPR) schedule based on Mach number, up to M=1.2
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