Numerical simulation of nozzle flow field with jet vane thrust vector control

2009 ◽  
Vol 224 (5) ◽  
pp. 541-548 ◽  
Author(s):  
M S R C Murty ◽  
M S Rao ◽  
D Chakraborty
Keyword(s):  
Numerical Simulation ◽  
Flow Field ◽  
Vector Control ◽  
Nozzle Flow ◽  
Thrust Vector Control ◽  
Thrust Vector

Experimental research and numerical simulations of thrust vector control nozzle flow

2016 ◽  
Vol 120 (1229) ◽  
pp. 1153-1174 ◽  
Author(s):  
S. Zivkovic ◽  
M. Milinovic ◽  
N. Gligorijevic ◽  
M. Pavic
Keyword(s):  
Vector Control ◽  
Gas Flow ◽  
Flow Dynamics ◽  
Nozzle Flow ◽  
Thrust Vector Control ◽  
Hardware System ◽  
Flow Test ◽  
Flow Geometry ◽  
Thrust Vector

ABSTRACTRocket motor nozzle flow geometry is considered through its influence on the thrust vector control (TVC) performances. Extensive research is conducted using theoretical and software simulations and compared with experimental results. Cold and hot flow test equipments are used. The main objective of the research is to establish the methodology of flow geometry optimisation on the TVC hardware system. Several geometry parameters are examined in detail and their effects on the system performances are presented. The discovered effects are used as guidelines in the TVC system design process. A numerical method is presented for the determination of dynamic response time upper limit for the TVC system based on the gas flow dynamics performances.

Numerical Simulation of Thrust Vector Control for a 2D Nozzle

2014 ◽  
Vol 494-495 ◽  
pp. 420-423
Author(s):  
Bo Wang ◽  
Yu Ge An ◽  
Man Zhang ◽  
Yuan Zheng
Keyword(s):  
Magnetic Field ◽  
Numerical Simulation ◽  
Vector Control ◽  
Cfd Simulation ◽  
Traditional Methods ◽  
Thrust Vector Control ◽  
Thrust Vector ◽  
The Magnetic Field

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.

scholarly journals Closed-loop actuator identification for Brazilian Thrust Vector Control development

2016 ◽  
Vol 49 (17) ◽  
pp. 468-473 ◽  
Author(s):  
Timo Wekerle ◽  
Euler Gonçalves Barbosa ◽  
César Moura Batagini ◽  
Luís E.V. Loures da Costa ◽  
Luís Gonzaga Trabasso
Keyword(s):  
Vector Control ◽  
Closed Loop ◽  
Thrust Vector Control ◽  
Thrust Vector
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