Simulation of aircraft wake vortex using pressure-based unified numerical approach for incompressible and compressible flows

Physics

• Eddy 100%
• Wakes 100%
• Advection 75%
• Simulation 75%
• Calculation 75%
• Pressure 50%
• Splitting 50%
• Navier-Stokes Equation 25%
• Mathematical Method 25%
• Poisson Equation 25%
• Charge Flow Device 25%
• Acoustic Wave 25%
• Pressure Gradient 25%
• Speed 25%
• Acoustics 25%

Engineering

• Compressible Flow 100%
• Advection 75%
• Simulation 75%
• Prediction 50%
• Good Agreement 25%
• Numerical Method 25%
• Pressure Gradient 25%
• Diffusive 25%
• Flow Regime 25%
• Navier-Stokes Equation 25%
• Numerical Approach 25%
• Vortex Flow 25%
• Rectangular Wing 25%
• Properties 25%
• Accuracy 25%
• Acoustics 25%
• Error 25%
• Validation 25%
• Aircraft 25%