Numerical research on two types of fluidic thrust vector

Engineering

• Fluidics 100%
• Expansion Ratio 100%
• Main Flow 100%
• Flaps 50%
• Computational Fluid Dynamics 50%
• Flow Distribution 50%
• Convergent 50%
• Relative Position 50%
• Flow in Nozzles 50%
• Survivability 50%
• Fighter Aircraft 50%
• Secondary Mass 50%
• Inlet Nozzle 50%
• Detectability 50%