Simulation of flow separation at the wing-body junction with different fairings

Engineering

• Flow Separation 100%
• Viscous Flow 66%
• Flow Solver 66%
• Numerical Study 33%
• Experimental Measurement 33%
• Boundary Layer 33%
• Navier-Stokes Equation 33%
• Eigenvalue 33%
• Jacobian Matrix 33%
• Aerodynamic Performance 33%
• Flow Region 33%
• Flux Vector 33%
• Drag Ratio 33%
• Local Time 33%
• Equation Turbulence Model 33%
• Residual Smoothing 33%
• Advancing Front Method 33%
• Tetrahedral Mesh 33%
• Flux Jacobian 33%