Investigation of "loud" modes in a high-speed jet to identify noise-producing events

Engineering

• Flow Field 100%
• Experimental Result 50%
• Particle Image Velocimetry 50%
• Axisymmetric 50%
• Closed Loop Control 50%
• Field Pressure 50%
• Velocity Field 50%
• Flow Physic 50%
• Control Algorithm 50%
• Acoustic Far Field 50%
• Noise Field 50%
• Anechoic Chamber 50%
• Noise Suppression 50%

Keyphrases

• Field Velocity 50%
• Fully Compressible 50%
• Noise Generation 50%
• Closed-loop Control Algorithm 50%