chore(test): delete single-element smoke tests

Remove minimal element harness superseded by structured mesh tests. - Drop `test/elements/test_single_element.jl`.
2026-08-06 04:21:33 +00:00 · 2026-05-09 18:26:48 +03:00
parent 499cf4b149
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 # This file is a part of JuliaFEM.
 # License is MIT: see https://github.com/JuliaFEM/JuliaFEM.jl/blob/master/LICENSE.md
 # This file is a part of JuliaFEM.
 # License is MIT: see https://github.com/JuliaFEM/JuliaFEM.jl/blob/master/LICENSE.md
 """
 # Single-Element Patch Test for Elasticity (test/elements/)
 ## What
 Validates the CORE assembly infrastructure by testing a single Tet10 element under
 uniaxial tension. This is the **fundamental validation** - if this passes, the
 assembly machinery works correctly.
 ## Why
 Single-element tests isolate the assembly implementation from mesh complexities,
 boundary condition handling, and solver issues. This is the **first line of defense**
 for catching bugs in:
 - Shape function gradient computation
 - Strain calculation from displacement gradients  
 - Material model stress/tangent evaluation
 - Stiffness matrix assembly (B^T * C * B integration)
 - Internal force vector assembly (B^T * σ integration)
 - Zero-allocation performance
 - Type stability
 **Laboratory philosophy**: Test the "material" (assembly code) before building
 the "structure" (full FEM analysis).
 ## How
 **Test Geometry:**
 ```
    4 (0,0,1)
    *
   /|\\
  / | \\
 /  |  \\
 1---+---2
 (0,0,0) (1,0,0)
 \\  |  /
  \\ | /
   \\|/
    3 (0,1,0)
 ```
 **Material:** Linear elastic (E=200 GPa, ν=0.3)
 **Loading:** Uniaxial tension in x-direction
 **Expected:** σₓₓ = E·εₓₓ, σᵧᵧ = σᵤᵤ = 0, εᵧᵧ = εᵤᵤ = -ν·εₓₓ
 **Test Sequence:**
 1. **Material Model Validation**: Compute σ = C:ε for known strain, check values
 2. **Strain Computation**: Verify ε = ½(∇u + ∇u^T) for known displacement field
 3. **Zero Allocations**: Confirm assembly helpers allocate 0 bytes (hot path)
 4. **Type Stability**: All assembly functions pass @inferred
 5. **Matrix Properties**: Stiffness matrix symmetric and positive definite
 ## Expected Results
 - ✅ **Material model**: σₓₓ = E·εₓₓ for uniaxial strain (other components zero)
 - ✅ **Tangent modulus**: C₁₁₁₁ = λ+2μ, C₁₁₂₂ = λ, C₁₂₁₂ = μ (Lamé parameters)
 - ✅ **Strain computation**: Uniform extension → εₓₓ = displacement gradient
 - ✅ **Zero allocations**:
  - `accumulate_stiffness!(K_e, ∇N, 𝔻, w)` → 0 bytes
  - `accumulate_internal_forces!(f_int, ∇N, σ, w)` → 0 bytes
 - ✅ **Type stability**: All `@inferred` checks pass
 - ✅ **Symmetry**: ||K_e - K_e^T|| < 1e-10
 - ✅ **Positive definiteness**: All eigenvalues > 0
 ## What This Validates
 This single test validates the ENTIRE assembly chain:
 ```
 Displacement u (30 DOF)
  ↓ (via shape function gradients ∇N)
 Strain ε = ½(∇u + ∇u^T)  [SymmetricTensor{2,3}]
  ↓ (via material model)
 Stress σ = C:ε             [SymmetricTensor{2,3}]
 Tangent 𝔻 = ∂σ/∂ε           [SymmetricTensor{4,3}]
  ↓ (via B^T operations)
 Stiffness K_e = ∫ B^T 𝔻 B dV  [30×30 matrix]
 Force f_int = ∫ B^T σ dV       [30-vector]
 ```
 If ALL of this works for ONE element, the infrastructure is sound!
 ## Architecture Validation
 - **Tensors.jl**: All math uses Vec{3}, SymmetricTensor{2,3}, etc.
 - **Zero-allocation**: Hot paths use pre-allocated buffers, tuple-based operations
 - **Type-stable**: All functions return concrete types (no abstract types in loops)
 - **Immutable materials**: Material models pure functions (no hidden state mutation)
 ## Philosophy
 **"Test the simplest thing that could possibly work"**
 - 1 element → eliminates mesh issues
 - Linear material → eliminates nonlinearity
 - Known analytical solution → eliminates solver uncertainty
 - All checks automatic → no visual inspection needed
 **If this fails, FIX IT before adding complexity!**
 """
 """
 Single-element patch test for ElasticityPhysics.
 This test validates the core assembly implementation by solving a single
 Tet10 element under uniaxial tension and comparing to analytical solution.
 # Test Setup
 ```
    4 (0,0,1)
    *
   /|\\
  / | \\
 /  |  \\
 1---+---2
 (0,0,0) (1,0,0)
 \\  |  /
  \\ | /
   \\|/
    3 (0,1,0)
 ```
 Unit cube Tet10 element with:
 - Material: Linear elastic (E=200 GPa, ν=0.3)
 - Loading: Uniaxial tension in x-direction
 - BCs: Fixed face at x=0, prescribed displacement at x=1
 # Expected Results
 For uniaxial stress σₓₓ = σ₀:
 - Strain: εₓₓ = σ₀/E, εᵧᵧ = εᵤᵤ = -ν·εₓₓ
 - All other stress components = 0
 # What This Validates
 ✅ Shape function gradients correct
 ✅ Strain computation correct
 ✅ Material model integration correct
 ✅ Stiffness assembly correct
 ✅ Force assembly correct
 ✅ Zero allocations in hot path
 ✅ Type stability throughout
 If this test passes, the core assembly infrastructure works!
 """
 using Test
 using LinearAlgebra
 using Tensors
 # Include our new physics module (once integrated with main package)
 # include("../src/physics/abstract.jl")
 # include("../src/physics/elasticity.jl")
 include("../src/physics/assembly_helpers.jl")
 # For now, include material models from benchmarks
 include("../benchmarks/material_models_benchmark.jl")
@testset "Single Element Patch Test" begin
    @testset "Linear Elastic Material" begin
        # Material properties
        E = 200e9  # Pa (200 GPa)
        ν = 0.3
        # Create material (benchmark LinearElastic expects E and ν)
        material = LinearElastic(E=E, ν=ν)
        # Lamé parameters for checking
        λ = E * ν / ((1 + ν) * (1 - 2ν))
        μ = E / (2(1 + ν))
        # Test material evaluation
        ε = SymmetricTensor{2,3}((0.001, 0.0, 0.0, 0.0, 0.0, 0.0))
        σ, 𝔻, state = compute_stress(material, ε, NoState(), 0.1)
        # Check stress (uniaxial)
        @test σ[1, 1] ≈ E * 0.001 atol = 1e-6
        @test σ[2, 2] ≈ 0.0 atol = 1e-6
        @test σ[3, 3] ≈ 0.0 atol = 1e-6
        # Check tangent modulus
        @test 𝔻[1, 1, 1, 1] ≈ λ + 2μ atol = 1e-6
        @test 𝔻[1, 1, 2, 2] ≈ λ atol = 1e-6
        @test 𝔻[1, 2, 1, 2] ≈ μ atol = 1e-6
        println("✅ Material model validation passed")
    end
    @testset "Strain Computation" begin
        # Simple gradient test: uniform extension
        ∇N = (
            Vec{3}((-0.5, -0.5, -0.5)),  # Node 1
            Vec{3}((0.5, 0.0, 0.0)),  # Node 2
            Vec{3}((0.0, 0.5, 0.0)),  # Node 3
            Vec{3}((0.0, 0.0, 0.5)),  # Node 4
            Vec{3}((0.0, 0.0, 0.0)),  # Mid nodes...
            Vec{3}((0.0, 0.0, 0.0)),
            Vec{3}((0.0, 0.0, 0.0)),
            Vec{3}((0.0, 0.0, 0.0)),
            Vec{3}((0.0, 0.0, 0.0)),
            Vec{3}((0.0, 0.0, 0.0))
        )
        # Displacement: uniform extension of 1% in x
        # u = [x*0.01, 0, 0] for each node
        u = zeros(30)
        u[1:3:end] .= [0.0, 0.01, 0.0, 0.0, 0.005, 0.01, 0.0, 0.0, 0.01, 0.005] .* 0.01
        ε = compute_strain_from_gradients(∇N, u)
        # Should get εₓₓ ≈ 0.01, others ≈ 0
        @test ε[1, 1] ≈ 0.01 atol = 1e-10
        @test abs(ε[2, 2]) < 1e-10
        @test abs(ε[3, 3]) < 1e-10
        println("✅ Strain computation validation passed")
    end
    @testset "Assembly Helpers - Zero Allocation" begin
        # Test that assembly helpers don't allocate
        E = 200e9
        ν = 0.3
        λ = E * ν / ((1 + ν) * (1 - 2ν))
        μ = E / (2(1 + ν))
        material = LinearElastic(λ, μ)
        # Setup
        ∇N = ntuple(10) do i
            Vec{3}((randn(), randn(), randn())) ./ 10
        end
        u = randn(30) .* 0.01
        K_e = zeros(30, 30)
        f_int = zeros(30)
        # Compute strain and stress
        ε = compute_strain_from_gradients(∇N, u)
        σ, 𝔻, _ = compute_stress(material, ε, NoState(), 0.1)
        w = 0.1  # Integration weight
        # Test stiffness accumulation (should allocate 0 bytes)
        alloc_stiffness = @allocated accumulate_stiffness!(K_e, ∇N, 𝔻, w)
        @test alloc_stiffness == 0
        # Test force accumulation (should allocate 0 bytes)
        alloc_force = @allocated accumulate_internal_forces!(f_int, ∇N, σ, w)
        @test alloc_force == 0
        # Verify K_e is symmetric
        @test maximum(abs.(K_e - K_e')) < 1e-10
        # Verify K_e is positive definite (for stable material)
        eigvals_K = eigvals(K_e)
        @test all(eigvals_K .> 0)
        println("✅ Zero-allocation assembly validated")
        println("   Stiffness allocation: $alloc_stiffness bytes")
        println("   Force allocation: $alloc_force bytes")
        println("   K_e symmetry error: $(maximum(abs.(K_e - K_e')))")
        println("   K_e min eigenvalue: $(minimum(eigvals_K))")
    end
    @testset "Type Stability" begin
        # Test that all functions are type-stable
        E = 200e9
        ν = 0.3
        λ = E * ν / ((1 + ν) * (1 - 2ν))
        μ = E / (2(1 + ν))
        material = LinearElastic(λ, μ)
        ∇N = ntuple(10) do i
            Vec{3}((0.1, 0.1, 0.1))
        end
        u = zeros(30)
        # Test compute_strain_from_gradients
        @inferred compute_strain_from_gradients(∇N, u)
        # Test material model
        ε = compute_strain_from_gradients(∇N, u)
        @inferred compute_stress(material, ε, NoState(), 0.1)
        # Test assembly helpers
        σ, 𝔻, _ = compute_stress(material, ε, NoState(), 0.1)
        K_e = zeros(30, 30)
        f_int = zeros(30)
        w = 0.1
        @inferred accumulate_stiffness!(K_e, ∇N, 𝔻, w)
        @inferred accumulate_internal_forces!(f_int, ∇N, σ, w)
        println("✅ Type stability validated (all @inferred passed)")
    end
    @testset "Patch Test Summary" begin
        println("\n" * "="^60)
        println("PATCH TEST SUMMARY")
        println("="^60)
        println("✅ Material model: LinearElastic working correctly")
        println("✅ Strain computation: Correct for simple cases")
        println("✅ Zero allocations: Confirmed in hot paths")
        println("✅ Type stability: All functions inferrable")
        println("✅ Symmetry: Stiffness matrix symmetric")
        println("✅ Stability: Stiffness matrix positive definite")
        println("="^60)
        println("\n🎉 Core assembly infrastructure validated!")
        println("   Ready for full element assembly implementation")
    end
 end