Efficient Aerodynamic Analysis of Air-Breathing Hypersonic Vehicle using Local Surface Inclination Method based on Unstructured Meshes

Engineering

• Aerodynamic Performance 100%
• Aerodynamic Analysis 100%
• Hypersonic Vehicle 100%
• Breathing 66%
• Good Agreement 33%
• Computational Fluid Dynamics 33%
• Skin-Friction Coefficient 33%
• Reference Temperature 33%
• Streamlines 33%
• Flow Passage 33%
• Isentropic 33%
• Local Skin 33%
• Reference Length 33%
• Air Breathing Propulsion 33%
• Tangent Wedge Method 33%
• Aerodynamic Coefficient 33%
• Design Phase 33%
• Flight Condition 33%
• Internal Flow 33%