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Unsteady turbomachinery computations using massively parallel platforms

Version 2 2024-06-04, 05:49
Version 1 2017-05-10, 15:56
conference contribution
posted on 2024-06-04, 05:49 authored by E Van Der Weide, G Kalitzin, J Schlüter, JJ Alonso
The CPU power offered by the latest generation of supercomputers is such that the unsteady simulation of the full wheel of a compressor or turbine is now within reach. This CPU power is mainly obtained by increasing the number of processors beyond several thousands, e.g. the BlueGene/L computer of Lawrence Livermore National Laboratory has approximately 130,000 processors. Consequently extreme care must be taken when the simulation codes are ported to these platforms. This paper discusses the computer scientific aspects of simulating unsteady turbomachinery flows on massively parallel systems when multi-block structured grids are used. Load balance, parallel IO and search algorithms are addressed, especially for the case where the number of processors is larger than the number of blocks, i.e. when blocks must be split during runtime. Preliminary results for cases with more than 200 million nodes running on 1,800 processors are presented.

History

Volume

7

Pagination

4904-4919

Location

Reno, Nevada

Start date

2006-01-09

End date

2006-01-12

ISBN-10

1563478072

Publication classification

E1.1 Full written paper - refereed

Title of proceedings

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Event

Aerospace Sciences Meeting and Exhibit (44th : 2006 : Reno, Nevada)

Publisher

American Institute of Aeronautics and Astronautics

Place of publication

Reston, VA.

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