Switching mechanism investigation for the supersonic jet element: Deflection, attachment and adjustment stages

Engineering

• Vortex 100%
• Flow Characteristics 50%
• Flow Simulation 50%
• Main Reason 50%
• Boundary Condition 50%
• Internal Flow 50%
• Control Flow 50%
• Static Pressure 50%
• Change Process 50%
• Switching Time 50%
• Viscous Flow 50%
• Channel Output 50%
• Left Side 50%
• Force Variation 50%
• Source Gas 50%
• Primary Jet 50%
• Coanda Effect 50%