Research
Computational Fluid Dynamics (CFD) Results
Pressure contour of an airfoil in supersonic flow. Through numerical simulation, we can accurately predict the pressure distribution on the aircraft surface, providing key data for aerodynamic design.
Computational Fluid Dynamics (CFD) Results
Velocity contour of an airfoil in supersonic flow. Through numerical simulation, we can accurately predict the velocity distribution on the aircraft surface, providing key data for aerodynamic design.
Mesh Structures
Structured grid around a complex geometry. High-quality mesh is the foundation for ensuring computational accuracy, especially when dealing with complex geometric boundaries.
More CFD Results
Numerical simulation of shock wave interaction on a hypersonic vehicle. This helps us understand the complex phenomena of the flow field under extreme flight conditions.
More Mesh Structures
Boundary layer mesh suitable for boundary layer simulation. By refining the mesh normal to the surface, the flow details within the boundary layer can be captured more accurately.