Numerical simulations of self-sustained oscillation characteristics in cavity with high-Mach-number flow disturbances

Engineering

• Aerodynamic Drag Reduction 33%
• Boundary Layer 33%
• Bow Shock 66%
• Cavity Pressure 33%
• Cavity Surface 33%
• Drag Coefficient 66%
• Drag Reduction 33%
• External Flow 33%
• Flow Distribution 100%
• Flow State 33%
• Gas Injection 66%
• High Mach Number 100%
• Initial Condition 33%
• Initial Phase 33%
• Internal Flow 33%
• Oscillation Characteristic 100%
• Oscillation Cycle 33%
• Oscillatory 33%
• Oscillatory Behavior 33%
• Peak Value 33%
• Stagnation Point 33%
• Sustained Oscillation 100%
• Temperature Region 33%
• Temporal Variation 33%
• Thermal Protection 66%
• Two Dimensional 33%