Add baroclinic instability test case

LibTrixi.jl/examples/libelixir_p4est3d_euler_baroclinic_instability.jl

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+# An idealized baroclinic instability test case
+#
+# Note that this libelixir is based on the original baroclinic instability elixir by
+# Erik Faulhaber for Trixi.jl
+# Source: https://github.com/trixi-framework/Trixi.jl/blob/main/examples/p4est_3d_dgsem/elixir_euler_baroclinic_instability.jl
+#
+# References:
+# - Paul A. Ullrich, Thomas Melvin, Christiane Jablonowski, Andrew Staniforth (2013)
+#   A proposed baroclinic wave test case for deep- and shallow-atmosphere dynamical cores
+#   https://doi.org/10.1002/qj.2241
+
+using OrdinaryDiffEq
+using Trixi
+using LinearAlgebra
+using LibTrixi
+
+
+# Initial condition for an idealized baroclinic instability test
+# https://doi.org/10.1002/qj.2241, Section 3.2 and Appendix A
+function initial_condition_baroclinic_instability(x, t,
+                                                  equations::CompressibleEulerEquations3D)
+    lon, lat, r = cartesian_to_sphere(x)
+    radius_earth = 6.371229e6
+    # Make sure that the r is not smaller than radius_earth
+    z = max(r - radius_earth, 0.0)
+
+    # Unperturbed basic state
+    rho, u, p = basic_state_baroclinic_instability_longitudinal_velocity(lon, lat, z)
+
+    # Stream function type perturbation
+    u_perturbation, v_perturbation = perturbation_stream_function(lon, lat, z)
+
+    u += u_perturbation
+    v = v_perturbation
+
+    # Convert spherical velocity to Cartesian
+    v1 = -sin(lon) * u - sin(lat) * cos(lon) * v
+    v2 = cos(lon) * u - sin(lat) * sin(lon) * v
+    v3 = cos(lat) * v
+
+    return prim2cons(SVector(rho, v1, v2, v3, p), equations)
+end
+
+function cartesian_to_sphere(x)
+    r = norm(x)
+    lambda = atan(x[2], x[1])
+    if lambda < 0
+        lambda += 2 * pi
+    end
+    phi = asin(x[3] / r)
+
+    return lambda, phi, r
+end
+
+# Unperturbed balanced steady-state.
+# Returns primitive variables with only the velocity in longitudinal direction (rho, u, p).
+# The other velocity components are zero.
+function basic_state_baroclinic_instability_longitudinal_velocity(lon, lat, z)
+    # Parameters from Table 1 in the paper
+    # Corresponding names in the paper are commented
+    radius_earth = 6.371229e6  # a
+    half_width_parameter = 2           # b
+    gravitational_acceleration = 9.80616     # g
+    k = 3           # k
+    surface_pressure = 1e5         # p₀
+    gas_constant = 287         # R
+    surface_equatorial_temperature = 310.0       # T₀ᴱ
+    surface_polar_temperature = 240.0       # T₀ᴾ
+    lapse_rate = 0.005       # Γ
+    angular_velocity = 7.29212e-5  # Ω
+
+    # Distance to the center of the Earth
+    r = z + radius_earth
+
+    # In the paper: T₀
+    temperature0 = 0.5 * (surface_equatorial_temperature + surface_polar_temperature)
+    # In the paper: A, B, C, H
+    const_a = 1 / lapse_rate
+    const_b = (temperature0 - surface_polar_temperature) /
+              (temperature0 * surface_polar_temperature)
+    const_c = 0.5 * (k + 2) * (surface_equatorial_temperature - surface_polar_temperature) /
+              (surface_equatorial_temperature * surface_polar_temperature)
+    const_h = gas_constant * temperature0 / gravitational_acceleration
+
+    # In the paper: (r - a) / bH
+    scaled_z = z / (half_width_parameter * const_h)
+
+    # Temporary variables
+    temp1 = exp(lapse_rate / temperature0 * z)
+    temp2 = exp(-scaled_z^2)
+
+    # In the paper: ̃τ₁, ̃τ₂
+    tau1 = const_a * lapse_rate / temperature0 * temp1 +
+           const_b * (1 - 2 * scaled_z^2) * temp2
+    tau2 = const_c * (1 - 2 * scaled_z^2) * temp2
+
+    # In the paper: ∫τ₁(r') dr', ∫τ₂(r') dr'
+    inttau1 = const_a * (temp1 - 1) + const_b * z * temp2
+    inttau2 = const_c * z * temp2
+
+    # Temporary variables
+    temp3 = r / radius_earth * cos(lat)
+    temp4 = temp3^k - k / (k + 2) * temp3^(k + 2)
+
+    # In the paper: T
+    temperature = 1 / ((r / radius_earth)^2 * (tau1 - tau2 * temp4))
+
+    # In the paper: U, u (zonal wind, first component of spherical velocity)
+    big_u = gravitational_acceleration / radius_earth * k * temperature * inttau2 *
+            (temp3^(k - 1) - temp3^(k + 1))
+    temp5 = radius_earth * cos(lat)
+    u = -angular_velocity * temp5 + sqrt(angular_velocity^2 * temp5^2 + temp5 * big_u)
+
+    # Hydrostatic pressure
+    p = surface_pressure *
+        exp(-gravitational_acceleration / gas_constant * (inttau1 - inttau2 * temp4))
+
+    # Density (via ideal gas law)
+    rho = p / (gas_constant * temperature)
+
+    return rho, u, p
+end
+
+# Perturbation as in Equations 25 and 26 of the paper (analytical derivative)
+function perturbation_stream_function(lon, lat, z)
+    # Parameters from Table 1 in the paper
+    # Corresponding names in the paper are commented
+    perturbation_radius = 1 / 6      # d₀ / a
+    perturbed_wind_amplitude = 1.0      # Vₚ
+    perturbation_lon = pi / 9     # Longitude of perturbation location
+    perturbation_lat = 2 * pi / 9 # Latitude of perturbation location
+    pertz = 15000    # Perturbation height cap
+
+    # Great circle distance (d in the paper) divided by a (radius of the Earth)
+    # because we never actually need d without dividing by a
+    great_circle_distance_by_a = acos(sin(perturbation_lat) * sin(lat) +
+                                      cos(perturbation_lat) * cos(lat) *
+                                      cos(lon - perturbation_lon))
+
+    # In the first case, the vertical taper function is per definition zero.
+    # In the second case, the stream function is per definition zero.
+    if z > pertz || great_circle_distance_by_a > perturbation_radius
+        return 0.0, 0.0
+    end
+
+    # Vertical tapering of stream function
+    perttaper = 1.0 - 3 * z^2 / pertz^2 + 2 * z^3 / pertz^3
+
+    # sin/cos(pi * d / (2 * d_0)) in the paper
+    sin_, cos_ = sincos(0.5 * pi * great_circle_distance_by_a / perturbation_radius)
+
+    # Common factor for both u and v
+    factor = 16 / (3 * sqrt(3)) * perturbed_wind_amplitude * perttaper * cos_^3 * sin_
+
+    u_perturbation = -factor * (-sin(perturbation_lat) * cos(lat) +
+                      cos(perturbation_lat) * sin(lat) * cos(lon - perturbation_lon)) /
+                     sin(great_circle_distance_by_a)
+
+    v_perturbation = factor * cos(perturbation_lat) * sin(lon - perturbation_lon) /
+                     sin(great_circle_distance_by_a)
+
+    return u_perturbation, v_perturbation
+end
+
+@inline function source_terms_baroclinic_instability(u, x, t,
+                                                     equations::CompressibleEulerEquations3D)
+    radius_earth = 6.371229e6  # a
+    gravitational_acceleration = 9.80616     # g
+    angular_velocity = 7.29212e-5  # Ω
+
+    r = norm(x)
+    # Make sure that r is not smaller than radius_earth
+    z = max(r - radius_earth, 0.0)
+    r = z + radius_earth
+
+    du1 = zero(eltype(u))
+
+    # Gravity term
+    temp = -gravitational_acceleration * radius_earth^2 / r^3
+    du2 = temp * u[1] * x[1]
+    du3 = temp * u[1] * x[2]
+    du4 = temp * u[1] * x[3]
+    du5 = temp * (u[2] * x[1] + u[3] * x[2] + u[4] * x[3])
+
+    # Coriolis term, -2Ω × ρv = -2 * angular_velocity * (0, 0, 1) × u[2:4]
+    du2 -= -2 * angular_velocity * u[3]
+    du3 -= 2 * angular_velocity * u[2]
+
+    return SVector(du1, du2, du3, du4, du5)
+end
+
+
+# The function to create the simulation state needs to be named `init_simstate`
+function init_simstate()
+
+    ###############################################################################
+    # Setup for the baroclinic instability test
+    gamma = 1.4
+    equations = CompressibleEulerEquations3D(gamma)
+
+    ###############################################################################
+    # semidiscretization of the problem
+
+    initial_condition = initial_condition_baroclinic_instability
+
+    boundary_conditions = Dict(:inside => boundary_condition_slip_wall,
+                               :outside => boundary_condition_slip_wall)
+
+    # This is a good estimate for the speed of sound in this example.
+    # Other values between 300 and 400 should work as well.
+    surface_flux = FluxLMARS(340)
+    volume_flux = flux_kennedy_gruber
+    solver = DGSEM(polydeg = 5, surface_flux = surface_flux,
+                   volume_integral = VolumeIntegralFluxDifferencing(volume_flux))
+
+    trees_per_cube_face = (16, 8)
+    mesh = Trixi.P4estMeshCubedSphere(trees_per_cube_face..., 6.371229e6, 30000.0,
+                                      polydeg = 5, initial_refinement_level = 0)
+
+    semi = SemidiscretizationHyperbolic(mesh, equations, initial_condition, solver,
+                                        source_terms = source_terms_baroclinic_instability,
+                                        boundary_conditions = boundary_conditions)
+
+    ###############################################################################
+    # ODE solvers, callbacks etc.
+
+    tspan = (0.0, 12 * 24 * 60 * 60.0) # time in seconds for 12 days#
+
+    ode = semidiscretize(semi, tspan)
+
+    summary_callback = SummaryCallback()
+
+    analysis_interval = 5000
+    analysis_callback = AnalysisCallback(semi, interval = analysis_interval)
+
+    alive_callback = AliveCallback(analysis_interval = analysis_interval)
+
+    save_solution = SaveSolutionCallback(interval = 5000,
+                                         save_initial_solution = true,
+                                         save_final_solution = true,
+                                         solution_variables = cons2prim,
+                                         output_directory = "out_baroclinic",)
+
+    callbacks = CallbackSet(summary_callback,
+                            analysis_callback,
+                            alive_callback,
+                            save_solution)
+
+
+    ###############################################################################
+    # create the time integrator
+
+    # OrdinaryDiffEq's `integrator`
+    # Use a Runge-Kutta method with automatic (error based) time step size control
+    integrator = init(ode, RDPK3SpFSAL49();
+                      abstol = 1.0e-6, reltol = 1.0e-6,
+                      ode_default_options()...,
+                      callback = callbacks,
+                      maxiters=5e5);
+
+    ###############################################################################
+    # Create simulation state
+
+    simstate = SimulationState(semi, integrator)
+
+    return simstate
+end