Aeronautical CFD in the age of petaflops-scale computing: from unstructured to Cartesian meshes
From MaRDI portal
Publication:1670037
DOI10.1016/j.euromechflu.2013.02.005zbMath1408.76002OpenAlexW1996201231MaRDI QIDQ1670037
Publication date: 4 September 2018
Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.euromechflu.2013.02.005
Lua error in Module:PublicationMSCList at line 37: attempt to index local 'msc_result' (a nil value).
Related Items (3)
A stable and non-dissipative kinetic energy and entropy preserving (KEEP) scheme for non-conforming block boundaries on Cartesian grids ⋮ Visualization of vortical flows in computational fluid dynamics ⋮ An efficient Cartesian mesh generation strategy for complex geometries
Cites Work
- Unnamed Item
- A versatile sharp interface immersed boundary method for incompressible flows with complex boundaries
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodies
- Improvements in the reliability and quality of unstructured hybrid mesh generation
- Drag prediction, decomposition and visualization in unstructured mesh CFD solver of TAS-code
- A hybrid building-block and gridless method for compressible flows
- Finite element flux-corrected transport (FEM-FCT) for the euler and Navier-Stokes equations
- Hybrid Prismatic/Tetrahedral Grid Generation for Viscous Flow Applications
- Some challenges of realistic flow simulations by unstructured grid CFD
- Large Scaled Computation of Incompressible Flows on Cartesian Mesh Using a Vector-Parallel Supercomputer
- Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids
This page was built for publication: Aeronautical CFD in the age of petaflops-scale computing: from unstructured to Cartesian meshes