Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers (Q1569372)
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scientific article; zbMATH DE number 1467899
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers |
scientific article; zbMATH DE number 1467899 |
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Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers (English)
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3 July 2000
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The authors consider the three-dimensional hypersonic viscous gas flow around a blunt body of complex geometry streamlined at an angle of attack. The principle of geometric parallelism is used to design a high-order accurate implicit finite difference scheme which is implemented on a network of different-power computers or on a distributed-memory multiprocessor computer.
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principle of geometric parallelism
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three-dimensional hypersonic viscous gas flow
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blunt body
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implicit finite difference scheme
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network of different-power computers
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distributed-memory multiprocessor computer
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angle of attack
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