Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8942091 | Computers & Fluids | 2018 | 15 Pages |
Abstract
Laminar shock-wave/boundary-layer interactions were simulated using OpenSBLI, a Python-based source code generation framework. Shock-capturing was performed by a 5th order finite-difference Weighted Essentially Non-Oscillatory (WENO)-Z scheme applied in characteristic space. Oblique shock conditions were imposed for a shock angle of θ=32.58â and Mach 2 free-stream, impinging on a laminar flat-plate boundary-layer. Performance of the code was assessed on different architectures for CPU, GPU and Xeon Phi.
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Authors
David J. Lusher, Satya P. Jammy, Neil D. Sandham,