Note: Output is not generated for this example (to save resources on GitHub).

Unsteady actuator case - 2D

In this example, an unsteady inlet velocity profile at encounters a wind turbine blade in a wall-less domain. The blade is modeled as a uniform body force on a thin rectangle.

using CairoMakie
using IncompressibleNavierStokes
using Random

Output directory

outdir = joinpath(@__DIR__, "output", "MultiActuator")

Floating point precision

T = Float64

Array type

ArrayType = Array
# using CUDA; ArrayType = CuArray
# using AMDGPU; ArrayType = ROCArray
# using oneAPI; ArrayType = oneArray
# using Metal; ArrayType = MtlArray

Boundary conditions

boundary_conditions = (
    # x left, x right
    (
        DirichletBC((dim, x, y, t) -> sinpi(sinpi(t / 6) / 6 + one(x) / 2 * (dim == 1))),
        PressureBC(),
    ),

    # y rear, y front
    (PressureBC(), PressureBC()),
)

Actuator body force: A thrust coefficient Cₜ distributed over a thin rectangle

create_bodyforce(; xc, yc, D, δ, C) =
    (dim, x, y, t) ->
        dim == 1 && abs(x - xc) ≤ δ / 2 && abs(y - yc) ≤ D / 2 ? -C / (D * δ) : zero(x)

create_manyforce(forces...) = function (dim, x, y, t)
    out = zero(x)
    for f in forces
        out += f(dim, x, y, t)
    end
    out
end

disk = (; D = T(1), δ = T(0.11), C = T(0.2))
bodyforce = create_manyforce(
    create_bodyforce(; xc = T(2), yc = T(0), disk...),
    create_bodyforce(; xc = T(4), yc = T(0.7), disk...),
    create_bodyforce(; xc = T(6.4), yc = T(-1), disk...),
)

A 2D grid is a Cartesian product of two vectors

n = 50
x = LinRange(T(0), T(10), 5n + 1), LinRange(-T(2), T(2), 2n + 1)
plotgrid(x...; figure = (; size = (600, 300)))

Build setup and assemble operators

setup = Setup(;
    x,
    Re = T(1000),
    boundary_conditions,
    bodyforce,
    issteadybodyforce = true,
    ArrayType,
);
nothing #hide

Initial conditions (extend inflow)

ustart = velocityfield(setup, (dim, x, y) -> dim == 1 ? one(x) : zero(x));
t = T(0)

boxes = map(bodyforce.forces) do (; xc, yc, D, δ)
    [
        Point2f(xc - δ / 2, yc + D / 2),
        Point2f(xc - δ / 2, yc - D / 2),
        Point2f(xc + δ / 2, yc - D / 2),
        Point2f(xc + δ / 2, yc + D / 2),
        Point2f(xc - δ / 2, yc + D / 2),
    ]
end
box = boxes[1]

Solve unsteady problem

state, outputs = solve_unsteady(;
    setup,
    ustart,
    tlims = (T(0), T(12)),
    method = RKMethods.RK44P2(),
    processors = (
        rtp = realtimeplotter(;
            setup,
            # plot = fieldplot,
            # fieldname = :velocitynorm,
            # fieldname = :pressure,
            size = (600, 300),
            nupdate = 1,
        ),
        boxplotter = processor() do state
            for box in boxes
                lines!(current_axis(), box; color = :red)
            end
        end,
        # ehist = realtimeplotter(; setup, plot = energy_history_plot, nupdate = 1),
        # espec = realtimeplotter(; setup, plot = energy_spectrum_plot, nupdate = 1),
        # anim = animator(; setup, path = "$outdir/vorticity.mkv", nupdate = 20),
        # vtk = vtk_writer(; setup, nupdate = 10, dir = "$outdir", filename = "solution"),
        # field = fieldsaver(; setup, nupdate = 10),
        log = timelogger(; nupdate = 100),
    ),
);
nothing #hide

Post-process

We may visualize or export the computed fields (u, p).

Export to VTK

save_vtk(state; setup, filename = joinpath(outdir, "solution"))

Plot pressure

fig = fieldplot(state; setup, size = (600, 300), fieldname = :pressure)
lines!.(boxes; color = :red);
fig

Plot velocity

fig = fieldplot(state; setup, size = (600, 300), fieldname = :velocitynorm)
lines!.(boxes; color = :red);
fig

Plot vorticity

fig = fieldplot(state; setup, size = (600, 300), fieldname = :vorticity)
lines!.(boxes; color = :red);
fig

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