Comparative analysis of corner separation controlled by steady jets and oscillating jets on a compressor cascade

Engineering

• Flow Distribution 100%
• Vorticity 100%
• Angle of Incidence 100%
• Comparative Analysis 100%
• Pressure Loss 100%
• Vortex Shedding 100%
• Vortex 50%
• Active Control 50%
• Trailing Edge 50%
• Structure Size 50%
• Excitation Frequency 50%
• Mode Dynamic 50%
• Blade Surface 50%
• Blade Loss 50%
• Loss Reduction 50%
• Limited Range 50%
• Main Mode 50%