Simple Example of a Simulation in jf1uids

Imports

import jax.numpy as jnp

from jf1uids import SimulationConfig
from jf1uids import SimulationParams
from jf1uids import get_helper_data
from jf1uids.fluid_equations.fluid import construct_primitive_state
from jf1uids import time_integration
from jf1uids.option_classes.simulation_config import finalize_config

from jf1uids.option_classes.simulation_config import OSHER, MINMOD
from jf1uids.option_classes.simulation_config import SPHERICAL

from jf1uids import get_registered_variables

import matplotlib.pyplot as plt

Simulation Setup

Let us set up a very simple simulation, mostly with default parameters.

First we get the configuration of the simulation, which contains parameters that typically do not change between simulations, changing which requires (just-in-time)-recompilation.

from jf1uids.option_classes.simulation_config import CARTESIAN, HLL, HLLC

config = SimulationConfig(
    geometry = CARTESIAN,
    limiter = OSHER,
    num_cells = 1001,
)

Next we setup the simulation parameters, things we might vary

params = SimulationParams(
    t_end = 0.2 # the typical value for a shock test
)

With this we generate some helper data, like the cell centers etc.

helper_data = get_helper_data(config)
registered_variables = get_registered_variables(config)

Next we setup the shock initial conditions, namely

(1)\[\begin{equation} \left(\begin{array}{l} \rho \\ u \\ p \end{array}\right)_L=\left(\begin{array}{l} 1 \\ 0 \\ 1 \end{array}\right), \quad\left(\begin{array}{l} \rho \\ u \\ p \end{array}\right)_R=\left(\begin{array}{c} 0.125 \\ 0 \\ 0.1 \end{array}\right) \end{equation}\]

with seperation at \(x=0.5\).

# setup the shock initial fluid state in terms of rho, u, p
shock_pos = 0.5
r = helper_data.geometric_centers
rho = jnp.where(r < shock_pos, 1.0, 0.125)
u = jnp.zeros_like(r)
p = jnp.where(r < shock_pos, 1.0, 0.1)

# get initial state
initial_state = construct_primitive_state(
    config = config,
    registered_variables = registered_variables,
    density = rho,
    velocity_x = u,
    gas_pressure = p
)

config = finalize_config(config, initial_state.shape)

Automatically setting open boundaries for Cartesian geometry.

Running the simulation

final_state = time_integration(initial_state, config, params, helper_data, registered_variables)
rho_final, u_final, p_final = final_state

Visualization

fig, axs = plt.subplots(1, 3, figsize=(15, 5))

axs[0].plot(r, rho, label='initial')
axs[0].plot(r, rho_final, label='final')
axs[0].set_title('Density')
axs[0].legend()

axs[1].plot(r, u, label='initial')
axs[1].plot(r, u_final, label='final')
axs[1].set_title('Velocity')
axs[1].legend()

axs[2].plot(r, p, label='initial')
axs[2].plot(r, p_final, label='final')
axs[2].set_title('Pressure')
axs[2].legend()

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