A parallel three-dimensional computational aeroacoustics method using non-linear disturbance equations

Keyphrases

• Three-dimensional (3D) 100%
• Computational Aeroacoustics 100%
• Nonlinear Disturbance Equations 100%
• Parallel Computer 66%
• Fourth Order 66%
• Acoustics 33%
• Average Flow 33%
• Inlet Conditions 33%
• Difference Basis 33%
• Domain Decomposition 33%
• Finite Difference 33%
• Spatial Discretization 33%
• Jet Noise 33%
• Axisymmetric Jet 33%
• Message Passing 33%
• Parallelizing 33%
• Parallel Performance 33%
• Runge-Kutta Scheme 33%
• Temporal Discretization 33%
• Decomposition Strategy 33%
• Instantaneous Flow 33%
• Flow Variables 33%
• Acoustic Variables 33%
• Conservative Form 33%
• Dispersion Relation Preserving Schemes 33%

Engineering

• Fourth Order 100%
• Axisymmetric 50%
• Domain Decomposition 50%
• Spatial Discretization 50%
• Dispersion Relation 50%
• Kutta Scheme 50%