Mason Shopperly

The Aguasabon Gorge from the air, dark water running out between forested rock walls.

Aerospace and mechanical engineer

CFD RL Researcher at AlignerrMEng, Aerospace Science and Engineering, UTIAS

Alberta, Canada

    From the governing equations to the hardware they end up in

    The problems are in fluids, in structures, in optimisation and estimation, and where those are coupled, as when a wing bends and twists under the load it is carrying.

    I write my own solvers and verify them against exact solutions, work across commercial, open-source and research codes, and report a result with the conditions under which it holds. Those answers have gone through design review with structures and manufacturing into parts that were built and flown.

    Available now · September 2026

    Open to engineering roles across that span: simulation and analysis, engineering software and systems, verification, and design that ends in hardware. Aerospace especially, and any technically demanding field. Calgary preferred, on-site or hybrid anywhere in Canada, and open to remote work.

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    One measurement, on the way in

    A shock tube, at the contact

    A shock tube is the standard first test of a compressible solver, because its exact answer is known on paper. Two schemes solve the same problem here. The dashed line is the exact density across the contact discontinuity; the two solid lines are what each scheme produced on the same mesh.

    This is one 1-D model problem at one grid spacing under one width rule, not a general ranking of the two schemes.

    The whole experiment, taken apart →

    • Exact
    • JST
    • Roe

    What was measured, in full →