Aeroelastic study of flexible flapping wings by a coupled lattice Boltzmann-finite element approach with immersed boundary method

Engineering

• Boltzmann Equation 100%
• Lateral Wind 100%
• Finite Element Method 100%
• Two Dimensional 50%
• Molecular Level 50%
• Computer Simulation 50%
• Numerical Approach 50%
• Takeoff 50%
• Computational Efficiency 50%
• Special Attention 50%
• Dynamic Structure 50%
• Lattice-Boltzmann Method 50%
• Interface Condition 50%
• Elastic Beam 50%
• Mesoscopic Scale 50%
• Flexible Wings 50%
• Discontinuous Galerkin 50%
• Macroscopic Quantity 50%
• Fluid-Structure Interaction 50%
• Harmonic Motion 50%