Prediction of Aircraft Surface Noise in Supersonic Cruise State

Engineering

• Sound Pressure Level 100%
• Aerodynamic Noise 100%
• Pressure Pulsation 100%
• Flow Distribution 50%
• Fatigue Damage 50%
• Acoustic Source 50%
• External Flow 50%
• Internal Flow 50%
• Jet Nozzle 50%
• Main Source 50%
• Aerodynamic Surface 50%
• Statistical Average 50%
• Exhaust Systems (Engine) 50%