Numerical investigation of wall cooling and suction effects on supersonic flat-plate boundary layer transition using large eddy simulation

Engineering

• Large Eddy Simulation 100%
• Flat Plate Boundary Layer 100%
• Boundary Layer Transition 100%
• Mach Number 50%
• Engineering 50%
• Flow Field 50%
• Boundary Layer 50%
• Coherent Structure 50%
• Velocity Profile 50%
• Drag Reduction 50%
• Hypersonic Vehicles 50%
• Cutting Edge 50%
• Flat Plate 50%

Physics

• Large Eddy Simulation 100%
• Supersonics 100%
• Flat Plate 100%
• Boundary Layer Transition 100%
• Flow Distribution 50%
• Boundary Layer 50%
• Drag Reduction 50%
• Mach Number 50%
• Aerodynamic Heating 50%
• Hypersonic Aircraft 50%
• Supersonic Boundary Layer 50%