Elimination of numerical damping in the stability analysis of non-compact thermoacoustic systems with linearized euler equations

Keyphrases

• Stability Analysis 100%
• Noncompact 100%
• Linearized Euler Equations 100%
• Numerical Damping 100%
• Thermoacoustic System 100%
• Combustor 50%
• Transversal 50%
• Effective Method 50%
• Eigenmodes 50%
• Thermodynamics 50%
• Munich 50%
• Technical University 50%
• Non-physical 50%
• Operation Point 50%
• Computational Fluid Dynamics 50%
• Stable Solutions 50%
• Numerical Stability 50%
• Eigenfrequency 50%
• Computational Aeroacoustics 50%
• Gas Turbine Combustion Chamber 50%
• Vortex Shedding 50%
• Premixed 50%
• Stability Results 50%
• Stabilized Finite Element Method 50%
• Stability Prediction 50%
• Swirl-stabilized 50%
• Physical Impacts 50%
• Viscothermal Losses 50%
• Induced Vortex 50%
• Diffusion Scheme 50%
• Artificial Diffusion 50%
• Acoustic Boundary Layer 50%
• Unstable Oscillation 50%

Engineering

• Linearized Euler Equation 100%
• Stability Analysis 100%
• Combustor 50%
• Boundary Layer 50%
• Eigenmode 50%
• Computational Fluid Dynamics 50%
• Eigenfrequencies 50%
• Gas Turbine Combustion 50%
• Vortex Shedding 50%
• Finite Element Analysis 50%
• Combustion Chamber 50%