Hypersonic Aerothermal Computations of a Sharp Fin Interaction

Keyphrases

• Low Reynolds number 100%
• Flow Field 100%
• 6-high 100%
• High Reynolds number 100%
• Hypersonic 100%
• Conjugate Heat Transfer 100%
• Aero-thermal 100%
• PRECICE 100%
• Inceptive 100%
• Steady State 50%
• Thermal Fluid 50%
• Thermomechanical 50%
• Flow Condition 50%
• Rapid Relaxation 50%
• Peak Pressure 50%
• Shock Wave Boundary Layer Interaction 50%
• Heat Transfer Rate 50%
• Structural Simulation 50%
• Skin Friction 50%
• State Interactions 50%
• Reynolds-averaged Navier-Stokes 50%
• Sudden Shift 50%
• Wall Pressure 50%
• Impinging Jet 50%
• Flat Plate Boundary Layer 50%
• Unit Reynolds number 50%
• Adapter 50%
• Corner Vortex 50%
• Boundary Layer Height 50%
• Thermal-structural 50%
• Stanton number 50%
• Physical Time 50%
• Aerothermoelastic 50%
• Thermal Compliance 50%

Engineering

• High Reynolds Number 100%
• Reynolds' Number 50%
• Vortex 50%
• Azimuthal 50%
• Boundary Layer 50%
• Empirical Model 50%
• Flow Condition 50%
• Peak Pressure 50%
• Layer Interaction 50%
• Skin-Friction Coefficient 50%
• Wall-Pressure 50%
• Reynolds-Averaged Navier-Stokes 50%
• Speed Fluid 50%
• Flat Plate Boundary Layer 50%
• Stanton Number 50%