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Laminar shock-wave/boundary-layer interactions were simulated using OpenS-BLI, a Python-based source code generation framework. Shock-capturing was performed by a 5 th 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 = 32.58 • 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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