An alternative method to calculate cross-flow instabilities

Engineering

• Flow Instability 100%
• Airfoil 66%
• Computational Fluid Dynamics 33%
• Flow Distribution 33%
• Sweep Angle 33%
• Good Performance 33%
• Transition Point 33%
• Secondary Flow 33%
• Primary Flow 33%
• Base Flow 33%
• Higher Order Dynamic Mode Decomposition 33%