Investigation of accelerating non-slender delta-wing planforms at high angle of attack using lagrangian coherent structures

Engineering

• Airfoil 50%
• Angle-of-Attack 100%
• Coherent Structure 50%
• Control Flow 50%
• Field Data 50%
• Finite Time 50%
• Flow Field 100%
• Flow Visualization 50%
• High Reynolds Number 50%
• Lagrangian Coherent Structure 100%
• Lyapunov Exponent 50%
• Planforms 100%
• Slender Delta Wing 100%
• Vorticity 50%

Physics

• Airfoil 50%
• Angle of Attack 100%
• Planforms 100%

Keyphrases

• Axial Acceleration 100%
• Field Data Analysis 50%
• Topological Transformation 50%