Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers
Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers
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.
network of different-power computers, implicit finite difference scheme, Turbulent boundary layers, principle of geometric parallelism, angle of attack, Strings, distributed-memory multiprocessor computer, Parallel numerical computation, blunt body, three-dimensional hypersonic viscous gas flow, Finite difference methods applied to problems in fluid mechanics
network of different-power computers, implicit finite difference scheme, Turbulent boundary layers, principle of geometric parallelism, angle of attack, Strings, distributed-memory multiprocessor computer, Parallel numerical computation, blunt body, three-dimensional hypersonic viscous gas flow, Finite difference methods applied to problems in fluid mechanics