Improved hybrid model for transitional separated flows over a rough compressor blade

Engineering

• Boundary Layer Transition 66%
• Compressor Blade 100%
• Computational Cost 33%
• Flow Region 33%
• Flow Separation 33%
• Hybrid Model 100%
• Induced Roughness 33%
• Laminar Flows 33%
• Laminar Separation Bubble 33%
• Modeling Strategy 33%
• Reattachment 33%
• Roughness Effect 33%
• Separated Flow 100%
• Simulation Method 33%
• Simulation Model 66%
• Subsonic Flow 33%
• Turbulent Flow 66%