Parallel aeroacoustic computation of unsteady transonic weapon bay using detached-eddy simulation via open computational fluid dynamics source codes

Keyphrases

• Aeroacoustics 100%
• Cavity Flow 25%
• Clock Time 25%
• Cluster Studies 25%
• Code-based 25%
• Computational Aeroacoustics 25%
• Computational Cost 25%
• Computational Fluid Dynamics 100%
• Detached Eddy Simulation 100%
• Dynamic Code 25%
• Dynamic Source 100%
• Fighter Aircraft 25%
• Finite Volume Method 25%
• Flow Studies 25%
• High-performance Computing Cluster 75%
• High-performance Simulation 25%
• Length-to-depth Ratio 25%
• Mach number 25%
• OpenFOAM 25%
• Reynolds number 25%
• Simulation Study 25%
• Source Code 100%
• Technology Advancement 25%
• Timing Analysis 25%
• Transonic 100%
• Weapons Bay 100%

Engineering

• Cavity Flow 25%
• Computational Cost 25%
• Computational Fluid Dynamics 100%
• Depth Ratio 25%
• Detached Eddy Simulation 100%
• Fighter Aircraft 25%
• Finite Volume Method 25%
• Flow Domain 25%
• Mach Number 25%
• Reynolds' Number 25%
• Technology Advancement 25%
• Time Analysis 25%

Physics

• Cavity Flow 25%
• Computational Aeroacoustics 25%
• Computational Fluid Dynamics 100%
• Mach Number 25%
• OpenFOAM 25%
• Reynolds Number 25%
• Transonic Flow 100%