Numerical Simulation of Thrust Vector Control for a 2D Nozzle
2014 ◽
Vol 494-495
◽
pp. 420-423
Keyword(s):
In modern campaign, Aircraft maneuverability and agility have been playing an increasingly important role. Plasma thrust vector control can avoid shortcomings of traditional methods, it has a very good prospect.In present work a CFD simulation of a thrust vector control for a 2D nozzle is performed.The results showed that the change of the magnetic field can impress the vector turn of the nozzle flowfield.
2009 ◽
Vol 224
(5)
◽
pp. 541-548
◽
Keyword(s):
2002 ◽
Vol 16
(17n18)
◽
pp. 2345-2351
◽