Effects of unstable oblique modes on the acoustic filed in a supersonic plane turbulent jet

Keyphrases

• Acoustics 100%
• Jet Shear Layer 100%
• Plane Turbulent Jet 100%
• Phase Speed 66%
• Convective Mach number 66%
• 3D Structure 33%
• Three-dimensional (3D) 33%
• Two Dimensional 33%
• Numerical Results 33%
• Periodic Boundary Conditions 33%
• Streamwise 33%
• Emission Mechanism 33%
• Spatial Derivatives 33%
• Wave Generation 33%
• Span-wise 33%
• Physical Insights 33%
• Generation Mechanism 33%
• Navier-Stokes Characteristic Boundary Conditions 33%
• Higher Order Compact 33%
• Runge-Kutta Scheme 33%
• Centerline Velocity 33%
• Upwind Scheme 33%
• High-order Compact Scheme 33%
• 4th Order 33%
• Sound Radiation 33%
• Compressible Navier-Stokes Equations 33%
• Random Disturbance 33%
• Acoustic Emission 33%
• Plane Jet 33%
• Jet Flow 33%
• Upstream Disturbances 33%
• Acoustic Waves 33%
• Mach Wave 33%
• Disturbance Conditions 33%
• Rapid Evolution 33%
• Shear Layer 33%
• Time Advancement 33%

Engineering

• Shear Layer 100%
• Oblique Mode 100%
• Convective 50%
• Phase Speed 50%
• Mach Number 50%
• Boundary Condition 50%
• Dimensional Structure 25%
• Two Dimensional 25%
• Streamwise 25%
• Periodic Boundary 25%
• Spanwise Direction 25%
• Compressible Navier 25%
• Plane Jet 25%
• Sound Radiation 25%
• Acoustic Emission 25%
• Centerline Velocity 25%
• Mach Wave 25%
• Kutta Scheme 25%
• Navier-Stokes Equation 25%