Time-accurate Experimental Investigation of Hypersonic Inlet Buzz at Mach 5

Engineering

• Experimental Investigation 100%
• Duct 100%
• Rectangular Cross Section 50%
• Resonator 50%
• Frame Rate 50%
• Data Sample 50%
• Pressure Amplitude 50%
• Flow Field 50%
• Schlieren 50%
• Peak Pressure 50%
• Solid Wall 50%
• Closed End 50%
• Samplerate 50%
• Static Pressure 50%
• Shear Layer 50%
• Separated Flow 50%