Multiprocessing On Supercomputers For Computational Aerodynamics - Info and Reading Options
By Yarrow, Maurice and Mehta, Unmeel B
"Multiprocessing On Supercomputers For Computational Aerodynamics" and the language of the book is English.
“Multiprocessing On Supercomputers For Computational Aerodynamics” Metadata:
- Title: ➤ Multiprocessing On Supercomputers For Computational Aerodynamics
- Authors: Yarrow, MauriceMehta, Unmeel B
- Language: English
“Multiprocessing On Supercomputers For Computational Aerodynamics” Subjects and Themes:
- Subjects: ➤ EXTRATERRESTRIAL LIFE - PLANETS - SPACE FLIGHT - UNIVERSE - ASTRONOMY - RADIO TELESCOPES
Edition Identifiers:
- Internet Archive ID: nasa_techdoc_19900014050
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"Multiprocessing On Supercomputers For Computational Aerodynamics" Description:
The Internet Archive:
Very little use is made of multiple processors available on current supercomputers (computers with a theoretical peak performance capability equal to 100 MFLOPs or more) in computational aerodynamics to significantly improve turnaround time. The productivity of a computer user is directly related to this turnaround time. In a time-sharing environment, the improvement in this speed is achieved when multiple processors are used efficiently to execute an algorithm. The concept of multiple instructions and multiple data (MIMD) through multi-tasking is applied via a strategy which requires relatively minor modifications to an existing code for a single processor. Essentially, this approach maps the available memory to multiple processors, exploiting the C-FORTRAN-Unix interface. The existing single processor code is mapped without the need for developing a new algorithm. The procedure for building a code utilizing this approach is automated with the Unix stream editor. As a demonstration of this approach, a Multiple Processor Multiple Grid (MPMG) code is developed. It is capable of using nine processors, and can be easily extended to a larger number of processors. This code solves the three-dimensional, Reynolds averaged, thin-layer and slender-layer Navier-Stokes equations with an implicit, approximately factored and diagonalized method. The solver is applied to generic oblique-wing aircraft problem on a four processor Cray-2 computer. A tricubic interpolation scheme is developed to increase the accuracy of coupling of overlapped grids. For the oblique-wing aircraft problem, a speedup of two in elapsed (turnaround) time is observed in a saturated time-sharing environment.
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"Multiprocessing On Supercomputers For Computational Aerodynamics" is available for download from The Internet Archive in "texts" format, the size of the file-s is: 10.07 Mbs, and the file-s went public at Mon Jul 26 2010.
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