Automated Hexahedral Meshing with GridPro: Structured Meshes for Parametric Geometry Variants

Automated multiblock meshing using topology templates and point cloud mapping streamlines CFD workflows. By leveraging Radial Basis Function (RBF) morphing, this new method ensures accurate topology adaptation for design variants. Case studies on turbines, volutes, and compressors highlight its efficiency, reducing manual effort while maintaining high-quality grids.

Hexahedral mesh for a turbocharger compressor.

Enhancing Turbocharger Efficiency with CFD and Automated Meshing Tools

Optimizing compressor design is crucial for turbocharger efficiency. CFD-driven analysis refines aerodynamics, while structured meshing enhances accuracy. GridPro automates high-quality meshing for impellers and volutes, accelerating design iterations. By leveraging CFD and advanced meshing, engineers can achieve superior compressor performance, improving fuel economy, power output, and regulatory compliance in modern engines.

Plate-heat exchanger internal mesh using structured multiblock hexahedral grid (GridPro).

Fulfilling Platе Hеat Exchangеr Meshing Needs for CFD Analysis

Thе intricatе intеrnal flow channеls in-bеtwееn thе corrugatеd platеs of platе hеat еxchangеrs rеquirе top notch, flow alignеd mеshеs. Thе systеmatically organizеd hеxahеdral cеlls found in structurеd grids arе thе idеal choicе for simulating platе hеat еxchangеrs. GridPro’s еfficiеnt blocking tools facilitatе rapid grid gеnеration for thеsе complеx flow paths.

Block-adapted, shock-fitted structured grid for the Orion reentry capsule in hypersonic conditions, showing blocks precisely aligned with the shock surface and refined grid clustering near critical high-gradient regions for improved simulation accuracy.

Fast and Accurate Hypersonic CFD Simulations: Impact of Automatic Shock-Aligned Meshes

GridPro’s block-aligned shock-fitted grids revolutionize hypersonic CFD simulations by aligning mesh blocks with shock contours. This approach improves accuracy and reduces computational demands, providing precise shock resolution and efficient computation for simulations of reentry capsules, reentry vehicles, rockets, and hypersonic vehicles.