Centralized gradient-based reconstruction for wall modeled large eddy simulations of hypersonic boundary layer transition

Keyphrases

• Acoustic Waves 33%
• Benchmark Problems 33%
• Boundary Layer 33%
• Boundary Layer Separation 33%
• Central Schemes 33%
• Characteristic Space 66%
• Coarse Grid 33%
• Complex Flow 33%
• Compressible Euler Equations 33%
• Compressible Navier-Stokes Equations 33%
• Compression Ramp 66%
• Computational Cost 33%
• Conservative Variables 66%
• Flow Dynamics 33%
• Gradient Based Reconstruction 100%
• Hypersonic Boundary Layer Transition 100%
• Inviscid 33%
• Method Robustness 33%
• Numerical Dissipation 100%
• Oblique Shock 33%
• Primitive Variables 33%
• Reconstruction Scheme 33%
• Selective Treatment 33%
• Shock 33%
• Shock Impingement 33%
• Shock Tube 33%
• Taylor-Green Vortex 33%
• Three-dimensional (3D) 33%
• Two Dimensional 66%
• Upwinding 33%
• Viscous Shock Waves 33%
• Wall Heating 33%
• Wall Model 33%
• WMLES 100%

Engineering

• Benchmark Problem 50%
• Boundary Layer 50%
• Boundary Layer Separation 50%
• Boundary Layer Transition 100%
• Central Scheme 50%
• Coarse Grid 50%
• Compressible Navier 50%
• Computational Cost 50%
• Euler Equation 50%
• Flow Dynamics 50%
• Navier-Stokes Equation 50%
• Oblique Shock 50%
• Overprediction 50%
• Primitive Variable 50%
• Shock Impingement 50%
• Two Dimensional 100%
• Vortex 50%

Mathematics

• Boundary Layer 100%
• Characteristic Space 66%
• Computational Cost 33%
• Euler Equation 33%
• Navier-Stokes Equation 33%
• Superiority 33%