Coupled conjugate heat transfer simulation for a scramjet inlet at Mach 8

Keyphrases

• Finite Volume 100%
• Isolator 100%
• Non-faces 100%
• Conjugate Heat Transfer 100%
• Scramjet Inlet 100%
• Shock Wave Boundary Layer Interaction 50%
• Hypersonic Inlet 50%
• Vehicle Engineering 50%
• Vehicle Performance 50%
• Hypersonic Vehicle 50%
• Expected Outcomes 50%
• Two Dimensional 50%
• Heat Conduction 50%
• Thermal Response 50%
• Three Dimensional Simulation 50%
• Two-dimensional Simulation 50%
• Aero-thermal 50%
• Cylinder Test 50%
• Compressible Flow Solver 50%
• Grid Constraints 50%

Engineering

• Nonconductor 100%
• Boundary Layer 50%
• Layer Interaction 50%
• Vehicle Design 50%
• Two Dimensional 50%
• Flow Solver 50%
• Compressible Flow 50%
• Hypersonic Vehicle 50%