Papers on computational fluid dynamics on GPUs
Running Unstructured Grid CFD Solvers on Modern Graphics Hardware Andrew Corrigan, Fernando Camelli, Rainald Löhner, and John Wallin, 19th AIAA Computational Fluid Dynamics Conference, July 21-24, 2009, San Antonio, TX, AIAA-2009-4001.
Code NACA0012 97K Elements NACA0012 193K Elements Missle 232K Elements
Techniques used to implement an unstructured grid solver on modern graphics hardware
are described. The three-dimensional Euler equations for inviscid, compressible flow are
considered. Effective memory bandwidth is improved by reducing total global memory
access and overlapping redundant computation, as well as using an appropriate numbering
scheme and data layout. The applicability of per-block shared memory is also considered.
The performance of the solver is demonstrated on two benchmark cases: a missile and the
NACA0012 wing. For a variety of mesh sizes, an average speed-up factor of roughly 9.5x
is observed over the equivalent parallelized OpenMP-code running on a quad-core CPU,
and roughly 33x over the equivalent code running in serial.