Parallel mesh adaptation for highly evolving geometries with application to solid propellant rockets

Keyphrases

• 3D Surface 50%
• Accurate Solution 50%
• Burnback 50%
• Configuration Change 50%
• Conservative Approach 50%
• Degree of Automation 50%
• Domain Boundary 50%
• Effective Surface 50%
• Gas Flow 50%
• Geometrical Features 50%
• Internal Gases 50%
• Mesh Modification 50%
• Mesh Quality 100%
• Mesh Smoothing 50%
• Modification Strategies 50%
• Novel Hybrids 50%
• Parallel Adaptive Mesh Refinement 100%
• Partitioner 50%
• Physical Systems 50%
• Propellant 50%
• Robust Surface 50%
• Solid Propellant Rocket 100%
• Solid Propellant Rocket Motor 50%
• Solution Transfer 50%
• Surface Mesh 50%
• Surface Wave Propagation 50%
• Topology Change 50%
• Volume Mesh 50%

Computer Science

• Configuration Change 100%
• Domain Boundary 100%
• Efficient Surface 100%
• Mesh Smoothing 100%
• Physical System 100%
• Regular Interval 100%
• Topology Change 100%

Material Science

• Gas Flow 50%
• Solid Propellant 100%