10,653 research outputs found
A local, un-structured, re-meshing technique capable of handling large body-motion in rotating machinery
In this paper we propose a simple, unstructured mesh generation technique that is capable of handling the large and complex blade motion that is encountered in certain rotating machines, such as vertical axis wind turbines or cycloidal propellers. The technique is characterised by localised re-meshing and interpolation, so as to keep the mesh generation cost and interpolation error as low as possible
Unstructured mesh algorithms for aerodynamic calculations
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The principle advantages of unstructured mesh strategies, as they relate to complex geometries, adaptive meshing capabilities, and parallel processing are emphasized. The various aspects required for the efficient and accurate solution of aerodynamic flows are addressed. These include mesh generation, mesh adaptivity, solution algorithms, convergence acceleration, and turbulence modeling. Computations of viscous turbulent two-dimensional flows and inviscid three-dimensional flows about complex configurations are demonstrated. Remaining obstacles and directions for future research are also outlined
Enhancing speed and scalability of the ParFlow simulation code
Regional hydrology studies are often supported by high resolution simulations
of subsurface flow that require expensive and extensive computations. Efficient
usage of the latest high performance parallel computing systems becomes a
necessity. The simulation software ParFlow has been demonstrated to meet this
requirement and shown to have excellent solver scalability for up to 16,384
processes. In the present work we show that the code requires further
enhancements in order to fully take advantage of current petascale machines. We
identify ParFlow's way of parallelization of the computational mesh as a
central bottleneck. We propose to reorganize this subsystem using fast mesh
partition algorithms provided by the parallel adaptive mesh refinement library
p4est. We realize this in a minimally invasive manner by modifying selected
parts of the code to reinterpret the existing mesh data structures. We evaluate
the scaling performance of the modified version of ParFlow, demonstrating good
weak and strong scaling up to 458k cores of the Juqueen supercomputer, and test
an example application at large scale.Comment: The final publication is available at link.springer.co
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