Files
rustytorch/crates/specialized/rtx-cfd/src/traits.rs
T
2026-03-04 00:08:42 +00:00

339 lines
9.8 KiB
Rust

// TDD: GREEN phase - Implement core traits to pass tests
use crate::error::CfdResult;
use nalgebra::{Scalar, Vector3};
use std::fmt::Debug;
/// Trait for fluid field data structures that hold velocity, pressure, and other flow variables
pub trait FluidField: Send + Sync + Debug {
/// Scalar type for field values (typically f32 or f64)
type Scalar: Scalar + Copy + Send + Sync + Debug;
/// Vector type for velocity fields
type Vector: Copy + Send + Sync + Debug;
/// Get velocity at a specific node/cell index
fn get_velocity(&self, index: usize) -> CfdResult<Self::Vector>;
/// Set velocity at a specific node/cell index
fn set_velocity(&mut self, index: usize, velocity: Self::Vector) -> CfdResult<()>;
/// Get pressure at a specific node/cell index
fn get_pressure(&self, index: usize) -> CfdResult<Self::Scalar>;
/// Set pressure at a specific node/cell index
fn set_pressure(&mut self, index: usize, pressure: Self::Scalar) -> CfdResult<()>;
/// Get total number of nodes/cells in the field
fn node_count(&self) -> usize;
/// Get temperature at a specific index (optional for thermal problems)
fn get_temperature(&self, _index: usize) -> CfdResult<Self::Scalar> {
// Default implementation for non-thermal problems - return zero (not implemented)
Err(crate::error::CfdError::InvalidParameter(
"Temperature not implemented for this field".to_string(),
))
}
/// Set temperature at a specific index (optional for thermal problems)
fn set_temperature(&mut self, _index: usize, _temperature: Self::Scalar) -> CfdResult<()> {
// Default implementation - do nothing for non-thermal problems
Ok(())
}
/// Get density at a specific index (for compressible flows)
fn get_density(&self, _index: usize) -> CfdResult<Self::Scalar> {
// Default implementation for incompressible flows - return error (not implemented)
Err(crate::error::CfdError::InvalidParameter(
"Density not implemented for this field".to_string(),
))
}
/// Set density at a specific index (for compressible flows)
fn set_density(&mut self, _index: usize, _density: Self::Scalar) -> CfdResult<()> {
// Default implementation - do nothing for incompressible flows
Ok(())
}
/// Check if all field values are finite and valid
fn validate(&self) -> CfdResult<()> {
for i in 0..self.node_count() {
let _velocity = self.get_velocity(i)?;
let _pressure = self.get_pressure(i)?;
// Add validation logic here if needed
}
Ok(())
}
}
/// Trait for CFD solvers (SIMPLE, PISO, LBM, etc.)
pub trait CfdSolver: Send + Sync + Debug {
/// Type of fluid field this solver operates on
type Field: FluidField;
/// Perform one solution step/iteration
/// Returns the residual (convergence measure)
fn solve_step(&mut self, field: &mut Self::Field, dt: f64) -> CfdResult<f64>;
/// Check if the solution has converged
fn is_converged(&self, residual: f64, tolerance: f64) -> bool;
/// Get current iteration count
fn get_iteration_count(&self) -> usize;
/// Reset solver state for a new simulation
fn reset(&mut self) -> CfdResult<()>;
/// Get solver name/type for diagnostics
fn solver_name(&self) -> &'static str {
"Generic CFD Solver"
}
/// Solve until convergence or maximum iterations
fn solve_to_convergence(
&mut self,
field: &mut Self::Field,
dt: f64,
tolerance: f64,
max_iterations: usize,
) -> CfdResult<(f64, usize)> {
self.reset()?;
for iteration in 0..max_iterations {
let residual = self.solve_step(field, dt)?;
if self.is_converged(residual, tolerance) {
return Ok((residual, iteration + 1));
}
}
Err(crate::error::CfdError::convergence(
max_iterations,
0.0, // We don't have the final residual here
tolerance,
))
}
/// Set solver parameters (optional)
fn set_parameters(&mut self, _params: &SolverParameters) -> CfdResult<()> {
Ok(())
}
}
/// Common solver parameters
#[derive(Debug, Clone)]
pub struct SolverParameters {
/// Convergence tolerance for residuals
pub tolerance: f64,
/// Maximum number of iterations allowed
pub max_iterations: usize,
/// Under-relaxation factor for stability
pub relaxation_factor: f64,
/// Time step size for transient simulations
pub time_step: f64,
}
impl Default for SolverParameters {
fn default() -> Self {
Self {
tolerance: 1e-6,
max_iterations: 1000,
relaxation_factor: 0.7,
time_step: 0.001,
}
}
}
/// Trait for mesh entities (cells, faces, nodes)
pub trait MeshEntity: Send + Sync + Debug {
/// Unique identifier for this entity
fn id(&self) -> usize;
/// Number of vertices/nodes that define this entity
fn vertex_count(&self) -> usize;
/// Indices of vertices that define this entity
fn vertex_indices(&self) -> &[usize];
/// Volume (for cells) or area (for faces) or 1.0 (for nodes)
fn volume(&self) -> f64;
/// Geometric centroid of the entity
fn centroid(&self) -> Vector3<f64>;
/// Entity type (cell, face, edge, node)
fn entity_type(&self) -> MeshEntityType {
match self.vertex_count() {
1 => MeshEntityType::Node,
2 => MeshEntityType::Edge,
3 => MeshEntityType::Triangle,
4 => MeshEntityType::Tetrahedron,
_ => MeshEntityType::Unknown,
}
}
/// Check if this entity is on the boundary
fn is_boundary(&self) -> bool {
false // Default implementation
}
}
/// Types of mesh entities
#[derive(Debug, Clone, Copy, PartialEq, Eq)]
pub enum MeshEntityType {
/// Point entity (0D)
Node,
/// Line entity (1D)
Edge,
/// Triangular face (2D)
Triangle,
/// Quadrilateral face (2D)
Quadrilateral,
/// Tetrahedral cell (3D)
Tetrahedron,
/// Hexahedral cell (3D)
Hexahedron,
/// Unknown or unsupported entity type
Unknown,
}
/// Trait for boundary conditions
pub trait BoundaryCondition: Send + Sync + Debug {
/// Type of field this boundary condition applies to
type Field: FluidField;
/// Apply the boundary condition to the field
fn apply(&self, field: &mut Self::Field, time: f64) -> CfdResult<()>;
/// Get the boundary condition type
fn bc_type(&self) -> BoundaryConditionType;
/// Get the boundary patch/region this applies to
fn boundary_patch(&self) -> &str;
/// Validate the boundary condition
fn validate(&self) -> CfdResult<()> {
Ok(())
}
}
/// Types of boundary conditions
#[derive(Debug, Clone, Copy, PartialEq, Eq)]
pub enum BoundaryConditionType {
/// Fixed velocity (Dirichlet)
FixedVelocity,
/// Fixed pressure (Dirichlet)
FixedPressure,
/// No-slip wall
NoSlipWall,
/// Slip wall
SlipWall,
/// Inlet with specified velocity
Inlet,
/// Outlet with specified pressure
Outlet,
/// Periodic boundary
Periodic,
/// Symmetry plane
Symmetry,
}
/// Trait for time integration schemes
pub trait TimeIntegrator: Send + Sync + Debug {
/// Type of field this integrator works with
type Field: FluidField;
/// Advance the field by one time step
fn advance(&mut self, field: &mut Self::Field, dt: f64) -> CfdResult<()>;
/// Get the integration scheme name
fn scheme_name(&self) -> &'static str;
/// Get the order of accuracy
fn order(&self) -> usize;
/// Check if the scheme is stable for the given time step
fn is_stable(&self, dt: f64, cfl_number: f64) -> bool;
}
/// Trait for turbulence models
pub trait TurbulenceModel: Send + Sync + Debug {
/// Type of field this model works with
type Field: FluidField;
/// Compute turbulent viscosity
fn compute_turbulent_viscosity(&self, field: &Self::Field) -> CfdResult<Vec<f64>>;
/// Update turbulence variables
fn update(&mut self, field: &mut Self::Field, dt: f64) -> CfdResult<()>;
/// Get the turbulence model name
fn model_name(&self) -> &'static str;
/// Get turbulence parameters
fn get_parameters(&self) -> TurbulenceParameters;
}
/// Turbulence model parameters
#[derive(Debug, Clone)]
pub struct TurbulenceParameters {
/// `C_μ` constant for k-ε model
pub c_mu: f64,
/// `C_ε1` constant for k-ε model
pub c_eps1: f64,
/// `C_ε2` constant for k-ε model
pub c_eps2: f64,
/// Schmidt number for turbulent kinetic energy
pub sigma_k: f64,
/// Schmidt number for turbulent dissipation rate
pub sigma_eps: f64,
}
impl Default for TurbulenceParameters {
fn default() -> Self {
// Standard k-epsilon model constants
Self {
c_mu: 0.09,
c_eps1: 1.44,
c_eps2: 1.92,
sigma_k: 1.0,
sigma_eps: 1.3,
}
}
}
#[cfg(test)]
mod tests {
use super::*;
#[test]
fn test_solver_parameters_default() {
let params = SolverParameters::default();
assert_eq!(params.tolerance, 1e-6);
assert_eq!(params.max_iterations, 1000);
assert_eq!(params.relaxation_factor, 0.7);
assert_eq!(params.time_step, 0.001);
}
#[test]
fn test_mesh_entity_type() {
assert_eq!(MeshEntityType::Node as u8, 0);
assert_ne!(MeshEntityType::Node, MeshEntityType::Edge);
}
#[test]
fn test_boundary_condition_type() {
assert_ne!(
BoundaryConditionType::FixedVelocity,
BoundaryConditionType::FixedPressure
);
}
#[test]
fn test_turbulence_parameters_default() {
let params = TurbulenceParameters::default();
assert_eq!(params.c_mu, 0.09);
assert_eq!(params.c_eps1, 1.44);
}
}