The evolution of interfaces for underwater supersonic gas jets

Engineering

• Nozzle Exit 100%
• Experimental Result 50%
• Transients 50%
• Obtains 50%
• Flow Field 50%
• Processing Method 50%
• Pressure Pulsation 50%
• Backpressure 50%
• Wake Flow 50%
• Kelvin Helmholtz Instability 50%