Aerodynamic performance research of micro flapping-wing in low Reynolds number flow

Engineering

• Aerodynamic Performance 100%
• Angle-of-Attack 66%
• Dual Time 33%
• Finite Volume Method 33%
• Key Parameter 33%
• Micro Air Vehicle 33%
• Navier-Stokes Equation 33%
• Numerical Method 33%
• Reynolds-Averaged Navier-Stokes 33%
• Spatial Discretization 33%