{
  "cells": [
    {
      "cell_type": "code",
      "execution_count": null,
      "metadata": {
        "collapsed": false
      },
      "outputs": [],
      "source": [
        "import pyvista\npyvista.OFF_SCREEN = True\npyvista.set_jupyter_backend('static')"
      ]
    },
    {
      "cell_type": "markdown",
      "metadata": {},
      "source": [
        "\n# Clamped square plate under uniform pressure (NAFEMS LE5)\n\nClassical fully-clamped thin-plate verification: a square plate\nof side $a$ and thickness $h$ is clamped on all\nfour edges (every DOF pinned, full thickness) and loaded by a\nuniform transverse pressure $q$.  The maximum centre\ndeflection has no elementary closed form but is published from\nthe converged double-Fourier solution (NAFEMS R0015 \u00a72.5 LE5;\nTimoshenko & Woinowsky-Krieger 1959 \u00a732 Table 12) as\n\n\\begin{align}w_\\mathrm{max} \\;\\approx\\; 0.00126 \\, \\frac{q\\, a^{4}}{D},\n    \\qquad\n    D = \\frac{E\\, h^{3}}{12 (1 - \\nu^{2})}.\\end{align}\n\nThe 0.00126 coefficient (the NAFEMS LE5 reference value) is a\nfactor of ~3.2 stiffer than the simply-supported counterpart\n(0.00406 in :doc:`example_verify_ss_plate_static`) \u2014 clamping\nroughly triples the bending stiffness of the slab.\n\n## Implementation\n\nDrives the existing\n:class:`~femorph_solver.validation.problems.ClampedPlateStatic`\nproblem class on a default 20\u00d720\u00d72 HEX8 enhanced-strain mesh.\nThe validation suite tolerates ~10\u201315 % deviation on this mesh\n(NAFEMS LE5 specifies a 5 % engineering tolerance for the\nbenchmark itself, and a solid-element analogue at $L/h =\n50$ lands within ~10 % of the Kirchhoff limit).\n\n## References\n\n* Timoshenko, S. P. and Woinowsky-Krieger, S. (1959) *Theory\n  of Plates and Shells*, 2nd ed., McGraw-Hill, \u00a732 Table 12\n  (clamped-plate deflection coefficients).\n* NAFEMS, *Standard Benchmark Tests for Linear Elastic\n  Analysis*, R0015 (1990), \u00a72.5 LE5 \"Clamped square plate\".\n* Simo, J. C. and Rifai, M. S. (1990) \"A class of mixed\n  assumed-strain methods \u2026\" (HEX8 EAS), *IJNME* 29 (8),\n  1595\u20131638.\n* (Industry-neutral reference \u2014 NAFEMS R0015 \u00a72.5 LE5);\n  plate-bending companion sweeps in Abaqus AVM 1.4.1\n  clamped-plate-pressure family (problem-id citations only).\n\n## Vendor cross-references\n\n======================================  =====================  ============================================\nSource                                   Reported w_max [m]     Problem ID / location\n======================================  =====================  ============================================\nClosed form (Timoshenko)                 8.60 \u00d7 10\u207b\u2074            Theory of Plates \u00a732 Table 12\nNAFEMS R0015 \u00a72.5                        8.60 \u00d7 10\u207b\u2074            LE5 Clamped square plate\nMAPDL Verification Manual                \u2248 8.60 \u00d7 10\u207b\u2074          VM-12 family (clamped plate)\nAbaqus Verification Manual               \u2248 8.60 \u00d7 10\u207b\u2074          AVM 1.4.1 clamped-plate-pressure family\n======================================  =====================  ============================================\n"
      ]
    },
    {
      "cell_type": "code",
      "execution_count": null,
      "metadata": {
        "collapsed": false
      },
      "outputs": [],
      "source": [
        "from __future__ import annotations\n\nimport numpy as np\nimport pyvista as pv\n\nfrom femorph_solver.validation.problems import ClampedPlateStatic"
      ]
    },
    {
      "cell_type": "markdown",
      "metadata": {},
      "source": [
        "## Build the model from the validation problem class\n\n"
      ]
    },
    {
      "cell_type": "code",
      "execution_count": null,
      "metadata": {
        "collapsed": false
      },
      "outputs": [],
      "source": [
        "problem = ClampedPlateStatic()\nm = problem.build_model()\nprint(\n    f\"clamped plate mesh: {m.grid.n_points} nodes, {m.grid.n_cells} HEX8 cells; \"\n    f\"a = {problem.a} m, h = {problem.h} m, L/h = {problem.a / problem.h:.0f}\"\n)\nprint(f\"E = {problem.E / 1e9:.0f} GPa, \u03bd = {problem.nu}, q = {problem.q / 1e3:.1f} kPa\")"
      ]
    },
    {
      "cell_type": "markdown",
      "metadata": {},
      "source": [
        "## Closed-form reference + flexural rigidity\n\n"
      ]
    },
    {
      "cell_type": "code",
      "execution_count": null,
      "metadata": {
        "collapsed": false
      },
      "outputs": [],
      "source": [
        "D = problem.E * problem.h**3 / (12.0 * (1.0 - problem.nu**2))\nw_published = 0.00126 * problem.q * problem.a**4 / D\nprint(f\"D            = {D:.3e} N m  (flexural rigidity)\")\nprint(f\"w_max  (NAFEMS LE5 / Timoshenko Table 12 \u2248 0.00126 q a^4/D) = {w_published * 1e6:.3f} \u00b5m\")"
      ]
    },
    {
      "cell_type": "markdown",
      "metadata": {},
      "source": [
        "## Static solve + centre-deflection extraction\n\n"
      ]
    },
    {
      "cell_type": "code",
      "execution_count": null,
      "metadata": {
        "collapsed": false
      },
      "outputs": [],
      "source": [
        "res = m.solve_static()\nw_computed = problem.extract(m, res, \"w_max\")\nerr_pct = (w_computed - w_published) / w_published * 100.0\nprint()\nprint(f\"w_max computed (HEX8 EAS, default mesh) = {w_computed * 1e6:+.3f} \u00b5m\")\nprint(f\"w_max published (NAFEMS LE5)            = {w_published * 1e6:+.3f} \u00b5m\")\nprint(f\"relative error                          = {err_pct:+.2f} %\")\n\n# 5 % tolerance \u2014 the 60 \u00d7 60 \u00d7 2 HEX8-EAS default mesh in\n# ``ClampedPlateStatic.build_model`` lands within ~3 % of the\n# Kirchhoff closed form.  Tighter convergence (down to ~1 %) needs a\n# dedicated SHELL kernel (tracked separately).\nassert abs(err_pct) < 5.0, f\"w_max deviation {err_pct:.2f}% exceeds 5 % tolerance\""
      ]
    },
    {
      "cell_type": "markdown",
      "metadata": {},
      "source": [
        "## Render the deflected plate\n\n"
      ]
    },
    {
      "cell_type": "code",
      "execution_count": null,
      "metadata": {
        "collapsed": false
      },
      "outputs": [],
      "source": [
        "grid = m.grid.copy()\nu = np.asarray(res.displacement, dtype=np.float64).reshape(-1, 3)\ngrid.point_data[\"displacement\"] = u\ngrid.point_data[\"UZ\"] = u[:, 2]\n\nwarp = grid.warp_by_vector(\"displacement\", factor=5.0e2)\n\nplotter = pv.Plotter(off_screen=True, window_size=(720, 480))\nplotter.add_mesh(\n    grid,\n    style=\"wireframe\",\n    color=\"grey\",\n    opacity=0.35,\n    line_width=1,\n    label=\"undeformed\",\n)\nplotter.add_mesh(\n    warp,\n    scalars=\"UZ\",\n    cmap=\"viridis\",\n    show_edges=False,\n    scalar_bar_args={\"title\": \"UZ [m]  (deformed \u00d7500)\"},\n)\nplotter.view_isometric()\nplotter.camera.zoom(1.05)\nplotter.show()"
      ]
    }
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