脉冲型流体振荡器射流对叶栅角区分离的控制研究

Engineering

• Vortex 100%
• Boundary Layer 100%
• Oscillator 100%
• Control System 50%
• Simulation Method 50%
• Trailing Edge 50%
• Suction Surface 50%
• Flow Velocity 50%
• Flow Rate 50%
• Chord Length 50%
• Incidence Angle 50%
• Aerodynamic Performance 50%
• Pressure Loss Coefficient 50%
• Static Pressure 50%
• Pressure Pulsation 50%
• Jet Flow Rate 50%
• Pressure Rise 50%
• Layer Development 50%