// 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; /// 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; /// 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 { // 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 { // 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; /// 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; /// 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>; /// 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); } }