Large-eddy simulation of supersonic flat-plate boundary layers using the monotonically integrated large-eddy simulation (MILES) technique

Engineering

• Simulation Technique 100%
• Flat Plate Boundary Layer 100%
• Heat Transfer Coefficient 66%
• Isothermal 66%
• Navier-Stokes Equation 66%
• Boundary Layer 33%
• Reynolds' Number 33%
• Good Agreement 33%
• Mach Number 33%
• Boundary Layer Thickness 33%
• Finite Volume Method 33%
• Inflow Boundary 33%
• Compressible Navier 33%
• Turbulent Stress 33%
• Prandtl Number 33%
• Skin-Friction Coefficient 33%
• Reynolds Analogy 33%
• Scale Model 33%

Keyphrases

• Large Eddy Simulation 100%
• Simulation Techniques 100%
• Flat Plate Boundary Layer 100%
• Heat Transfer Coefficient 50%
• Tetrahedron 25%
• Flow Field 25%
• Boundary Layer 25%
• Unstructured Grid 25%
• Navier-Stokes Equations 25%
• Reynolds number 25%
• Mach number 25%
• Boundary Layer Thickness 25%
• Finite Volume Method 25%
• Inflow Boundary 25%
• Second-order Accuracy 25%
• Numerical Dissipation 25%
• Skin Friction 25%
• Compressible Navier-Stokes Equations 25%
• Turbulent Stress 25%
• Friction Heat 25%
• Turbulent Prandtl number 25%
• Reynolds Analogy 25%
• Subgrid-scale Model 25%