Numerical Simulation of Thrust Vector Control for a 2D Nozzle

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Abstract:

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.

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420-423

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February 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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