Response of an annular burner nozzle to transverse acoustic excitation

Keyphrases

• Nozzle 100%
• Burner 100%
• Acoustic Excitation 100%
• Transverse Acoustics 100%
• Annular Jet 66%
• Combustor 33%
• Wave Structure 33%
• Long Wavelength 33%
• Boundary Layer 33%
• Large-scale Structure 33%
• Rocket 33%
• Standing Wave 33%
• Annulus 33%
• Acoustic Waves 33%
• Relative Strength 33%
• Land-based 33%
• Turbine Engine 33%
• Acoustic Disturbance 33%
• Transverse Excitation 33%
• Antinode 33%
• Pressure Node 33%
• High-frequency Oscillations 33%
• Transverse Mode 33%

Engineering

• Circumferential 100%
• Centerline 100%
• Nodes 50%
• Combustor 50%
• Vortex 50%
• Standing Wave 50%
• Boundary Layer 50%
• Relative Strength 50%
• Antinode 50%
• Vorticity 50%
• Turbine 50%

Physics

• Combustion Stability 100%
• Acoustic Excitation 100%