Investigation of supersonic underexpanded jets using adaptive unstructured finite elements

Engineering

• Axisymmetric 50%
• Eigenvalue 50%
• Error Estimate 50%
• Error Indicator 50%
• Euler Equation 50%
• Filtration 50%
• Fine Mesh 50%
• Finite Element Method 100%
• Implicit Method 50%
• Local Scale 50%
• Shear Layer 50%
• Simulation Method 50%
• Simulation Result 50%
• Velocity Gradient 50%

Keyphrases

• Mesh Generator 100%
• Over-expanded 100%
• Point Implicit 100%
• Supersonic Underexpanded Jet 100%
• Unstructured Finite Volume 100%