Identification of the aeroacoustic response of a low Mach number flow through a [formula omitted]-joint

Keyphrases

• Low Mach number Flow 100%
• Aeroacoustics 100%
• Two Dimensional 50%
• Shear Layer 50%
• Source Model 50%
• System Identification 50%
• Laminar Flow 50%
• Sound System 50%
• Low Mach number 50%
• Flow Computation 50%
• Incompressible Flow 50%
• Physical Mechanism 50%
• Confined Flow 50%
• Acoustic Excitation 50%
• Comparison with Experimental Results 50%
• Vortex Sound Theory 50%
• Sound Production 50%

Engineering

• Joints (Structural Components) 100%
• Low Mach Number 100%
• Experimental Result 33%
• Two Dimensional 33%
• Shear Layer 33%
• Source Model 33%
• Vortex 33%
• Laminar Flows 33%
• Incompressible Flow 33%