nanoHUB_remote_composite_laminate_example.ipynb

{
 "cells": [
  {
   "cell_type": "markdown",
   "metadata": {},
   "source": [
    "# Using the nanoHUB web API"
   ]
  },
  {
   "cell_type": "markdown",
   "metadata": {},
   "source": [
    "## Prerequisites\n",
    "In order to run a nanoHUB tool via the web API, you need a nanoHUB account and a registered web app.\n",
    "\n",
    "Create a nanoHUB account: https://nanohub.org/register/\n",
    "\n",
    "Register a web app: https://nanohub.org/developer/api/applications/new"
   ]
  },
  {
   "cell_type": "markdown",
   "metadata": {},
   "source": [
    "## Introduction"
   ]
  },
  {
   "cell_type": "markdown",
   "metadata": {},
   "source": [
    "This simple example notebook demonstrates use of the NanoHUB Composite-Laminate tool, called \"complam.\" The tool is more fully described here: https://nanohub.org/resources/complam.\n",
    "\n",
    "(add more detailed understanding here later...)"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 1,
   "metadata": {},
   "outputs": [],
   "source": [
    "from NanoHUB_remote import \\\n",
    "    authenticate, get_driver, launch_tool, get_results, extract_results"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 2,
   "metadata": {},
   "outputs": [],
   "source": [
    "# In mysecrets.py, set your web app and account secrets.\n",
    "# \n",
    "# Example, with user credentials:\n",
    "# auth_data = {\n",
    "#    'client_id': '',       # Get this when you register a web app\n",
    "#    'client_secret': '',   # Get this when you register a web app\n",
    "#    'grant_type': 'password',\n",
    "#    'username': '',        # Get this when you create a nanoHUB account\n",
    "#    'password': ''         # Get this when you create a nanoHUB account\n",
    "# }\n",
    "#\n",
    "# This design is strictly for convenience so that this notebook can be \n",
    "# shared without storing any secrets.\n",
    "from mysecrets import auth_data\n",
    "\n",
    "# Authenticate; use headers in all subsequent steps\n",
    "headers = authenticate(auth_data)"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 3,
   "metadata": {},
   "outputs": [],
   "source": [
    "# The short name of the nanoHUB tool to run; this is the final stanza of\n",
    "# the tool URL (e.g. https://nanohub.org/tools/complam)\n",
    "tool_name = 'complam'\n",
    "\n",
    "# Input values; keys are the labels of the inputs in the GUI\n",
    "tool_inputs = {\n",
    "    'E1': '132GPa',        # Longitudinal Young's Modulus\n",
    "    'E2': '12.9GPa',       # Transverse Young's Modulus (in-plane)\n",
    "    'h0': '0.23mm'         # Lamina thickness\n",
    "}"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 4,
   "metadata": {},
   "outputs": [],
   "source": [
    "# Generate the XML driver to run the tool with our inputs\n",
    "driver_json = get_driver(tool_name, tool_inputs, headers)"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 5,
   "metadata": {},
   "outputs": [],
   "source": [
    "# Start the simulation\n",
    "session_id = launch_tool(driver_json, headers)"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 6,
   "metadata": {},
   "outputs": [
    {
     "name": "stdout",
     "output_type": "stream",
     "text": [
      "1336474\n"
     ]
    }
   ],
   "source": [
    "# This is useful for debugging\n",
    "print session_id"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 7,
   "metadata": {
    "scrolled": true
   },
   "outputs": [],
   "source": [
    "# Get the results when available\n",
    "run_results = get_results(session_id, headers)"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 8,
   "metadata": {},
   "outputs": [],
   "source": [
    "# The outputs we want; these are the labels in the result selector in the\n",
    "# tool GUI \n",
    "outputs = ['Shear Modulus', 'Longitudinal Modulus']\n",
    "\n",
    "# Get the desired outputs\n",
    "results = extract_results(run_results, outputs)"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 9,
   "metadata": {},
   "outputs": [
    {
     "name": "stdout",
     "output_type": "stream",
     "text": [
      "{'Shear Modulus': 35021400000.0, 'Longitudinal Modulus': 23.44}\n"
     ]
    }
   ],
   "source": [
    "print results"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": 10,
   "metadata": {},
   "outputs": [
    {
     "name": "stdout",
     "output_type": "stream",
     "text": [
      "<?xml version=\"1.0\"?>\n",
      "<run>\n",
      "    <tool>\n",
      "        <id>complam</id>\n",
      "        <name>Composite Laminate Analysis</name>\n",
      "        <version>\n",
      "            <identifier>1.2x</identifier>\n",
      "            <application>\n",
      "                <revision>35</revision>\n",
      "                <modified>2016-04-20 02:31:05 -0400 (Wed, 20 Apr 2016)</modified>\n",
      "                <installed>2016-04-20 10:49:18 EDT</installed>\n",
      "                <directory id=\"top\">/apps/complam/r35</directory>\n",
      "                <directory id=\"tool\">/apps/complam/r35/rappture</directory>\n",
      "            </application>\n",
      "            <rappture>\n",
      "                <language>matlab</language>\n",
      "                <version>1.7</version>\n",
      "                <revision>6697</revision>\n",
      "                <modified>$LastChangedDate: 2016-05-04 14:27:36 -0400 (Wed, 04 May 2016) $</modified>\n",
      "            </rappture>\n",
      "        </version>\n",
      "        <title>Classical Laminate Plate Theory</title>\n",
      "        <command>run_main_clpt.sh @driver</command>\n",
      "        <uq>1</uq>\n",
      "        <cache>0</cache>\n",
      "    </tool>\n",
      "    <input>\n",
      "        <group id=\"tabs\">\n",
      "            <group id=\"Material\">\n",
      "                <about>\n",
      "                    <label>Material</label>\n",
      "                </about>\n",
      "                <number id=\"E1\">\n",
      "                    <about>\n",
      "                        <label>E1</label>\n",
      "                        <description>Longitudinal Young's Modulus</description>\n",
      "                    </about>\n",
      "                    <units>GPa</units>\n",
      "                    <min>0.0GPa</min>\n",
      "                    <max>500GPa</max>\n",
      "                    <default>138GPa</default>\n",
      "                    <current>132GPa</current>\n",
      "                </number>\n",
      "                <number id=\"E2\">\n",
      "                    <about>\n",
      "                        <label>E2</label>\n",
      "                        <description>Transverse Young's Modulus In-Plane</description>\n",
      "                    </about>\n",
      "                    <units>GPa</units>\n",
      "                    <min>0.0GPa</min>\n",
      "                    <max>500GPa</max>\n",
      "                    <default>14.5GPa</default>\n",
      "                    <current>12.9GPa</current>\n",
      "                </number>\n",
      "                <number id=\"nu12\">\n",
      "                    <about>\n",
      "                        <label>nu12</label>\n",
      "                        <description>Major In-Plane Poisson's Ratio</description>\n",
      "                    </about>\n",
      "                    <units/>\n",
      "                    <min>-1.0</min>\n",
      "                    <max>0.5</max>\n",
      "                    <default>0.21</default>\n",
      "                    <current>0.21</current>\n",
      "                </number>\n",
      "                <number id=\"G12\">\n",
      "                    <about>\n",
      "                        <label>G12</label>\n",
      "                        <description>Major In-Plane Shear Modulus</description>\n",
      "                    </about>\n",
      "                    <units>GPa</units>\n",
      "                    <min>0.0GPa</min>\n",
      "                    <max>500GPa</max>\n",
      "                    <default>5.86</default>\n",
      "                    <current>5.86</current>\n",
      "                </number>\n",
      "                <number id=\"alpha1\">\n",
      "                    <about>\n",
      "                        <label>alpha1</label>\n",
      "                        <description>Longitudinal Thermal Expansion Coefficient</description>\n",
      "                    </about>\n",
      "                    <units/>\n",
      "                    <min>-10e-6</min>\n",
      "                    <max>100e-6</max>\n",
      "                    <default>1e-6</default>\n",
      "                    <current>1e-6</current>\n",
      "                </number>\n",
      "                <number id=\"alpha2\">\n",
      "                    <about>\n",
      "                        <label>alpha2</label>\n",
      "                        <description>Transverse Thermal Expansion Coefficient</description>\n",
      "                    </about>\n",
      "                    <units/>\n",
      "                    <min>-10e-6</min>\n",
      "                    <max>100e-6</max>\n",
      "                    <default>30e-6</default>\n",
      "                    <current>30e-6</current>\n",
      "                </number>\n",
      "            </group>\n",
      "            <group id=\"Layup\">\n",
      "                <about>\n",
      "                    <label>Layup</label>\n",
      "                </about>\n",
      "                <number id=\"h0\">\n",
      "                    <about>\n",
      "                        <label>h0</label>\n",
      "                        <description>Lamina Thickenss</description>\n",
      "                    </about>\n",
      "                    <units>m</units>\n",
      "                    <min>0m</min>\n",
      "                    <max>10e-3m</max>\n",
      "                    <default>0.2286mm</default>\n",
      "                    <current>0.23mm</current>\n",
      "                </number>\n",
      "                <string id=\"theta\">\n",
      "                    <about>\n",
      "                        <label>theta</label>\n",
      "                        <description>Lamina Angle</description>\n",
      "                    </about>\n",
      "                    <default>[45,-45,-45,45]</default>\n",
      "                    <current>[45,-45,-45,45]</current>\n",
      "                </string>\n",
      "            </group>\n",
      "            <group id=\"Loading\">\n",
      "                <about>\n",
      "                    <label>Loading</label>\n",
      "                </about>\n",
      "                <number id=\"Nx\">\n",
      "                    <about>\n",
      "                        <label>Nx</label>\n",
      "                        <description>Applied Normal Edge Force in X-Direction</description>\n",
      "                    </about>\n",
      "                    <units>N/m</units>\n",
      "                    <min>-10000N/m</min>\n",
      "                    <max>10000N/m</max>\n",
      "                    <default>0N/m</default>\n",
      "                    <current>0N/m</current>\n",
      "                </number>\n",
      "                <number id=\"Ny\">\n",
      "                    <about>\n",
      "                        <label>Ny</label>\n",
      "                        <description>Applied Normal Edge Force in Y-Direction</description>\n",
      "                    </about>\n",
      "                    <units>N/m</units>\n",
      "                    <min>-10000N/m</min>\n",
      "                    <max>10000N/m</max>\n",
      "                    <default>0N/m</default>\n",
      "                    <current>0N/m</current>\n",
      "                </number>\n",
      "                <number id=\"Nxy\">\n",
      "                    <about>\n",
      "                        <label>Nxy</label>\n",
      "                        <description>Applied Edge Shear Force in XY-Direction</description>\n",
      "                    </about>\n",
      "                    <units>N/m</units>\n",
      "                    <min>-10000N/m</min>\n",
      "                    <max>10000N/m</max>\n",
      "                    <default>0N/m</default>\n",
      "                    <current>0N/m</current>\n",
      "                </number>\n",
      "                <number id=\"Mx\">\n",
      "                    <about>\n",
      "                        <label>Mx</label>\n",
      "                        <description>Applied Bending Moment about X-Axis</description>\n",
      "                    </about>\n",
      "                    <units>N</units>\n",
      "                    <min>-10000N</min>\n",
      "                    <max>10000N</max>\n",
      "                    <default>0N</default>\n",
      "                    <current>0N</current>\n",
      "                </number>\n",
      "                <number id=\"My\">\n",
      "                    <about>\n",
      "                        <label>My</label>\n",
      "                        <description>Applied Bending Moment about Y-Axis</description>\n",
      "                    </about>\n",
      "                    <units>N</units>\n",
      "                    <min>-10000N</min>\n",
      "                    <max>10000N</max>\n",
      "                    <default>0N</default>\n",
      "                    <current>0N</current>\n",
      "                </number>\n",
      "                <number id=\"Mxy\">\n",
      "                    <about>\n",
      "                        <label>Mxy</label>\n",
      "                        <description>Applied Twisting Moment</description>\n",
      "                    </about>\n",
      "                    <units>N</units>\n",
      "                    <min>-10000N</min>\n",
      "                    <max>10000N</max>\n",
      "                    <default>0N</default>\n",
      "                    <current>0N</current>\n",
      "                </number>\n",
      "                <number id=\"Ti\">\n",
      "                    <about>\n",
      "                        <label>Ti</label>\n",
      "                        <description>Initial Temperature</description>\n",
      "                    </about>\n",
      "                    <units>C</units>\n",
      "                    <min>-273.15C</min>\n",
      "                    <max>500C</max>\n",
      "                    <default>0C</default>\n",
      "                    <current>0C</current>\n",
      "                </number>\n",
      "                <number id=\"Tf\">\n",
      "                    <about>\n",
      "                        <label>Tf</label>\n",
      "                        <description>Final Temperature</description>\n",
      "                    </about>\n",
      "                    <units>C</units>\n",
      "                    <min>-273.15C</min>\n",
      "                    <max>500C</max>\n",
      "                    <default>0C</default>\n",
      "                    <current>0C</current>\n",
      "                </number>\n",
      "                <!--\n",
      "          <integer id=\"xRes\">\n",
      "              <about>\n",
      "                  <label>xRes</label>\n",
      "                  <description>Number of points in the x-direction where the solution will be evaluated</description>\n",
      "              </about>\n",
      "              <min>10</min>\n",
      "              <max>1001</max>\n",
      "              <default>51</default>  \n",
      "          </integer>\n",
      "\t  \n",
      "          <integer id=\"yRes\">\n",
      "              <about>\n",
      "                  <label>yRes</label>\n",
      "                  <description>Number of points in the y-direction where the solution will be evaluated</description>\n",
      "              </about>\n",
      "              <min>10</min>\n",
      "              <max>1001</max>\n",
      "              <default>51</default>  \n",
      "          </integer>\n",
      "          -->\n",
      "            </group>\n",
      "        </group>\n",
      "        <!-- This group of groups is drawn as a set of tabs -->\n",
      "    </input>\n",
      "    <output>\n",
      "        <string id=\"Ins\">\n",
      "            <current>E1 \t     1.32e+11 \n",
      " E2 \t     1.29e+10 \n",
      " nu12 \t         0.21 \n",
      " G12 \t         5.86 \n",
      " alpha1 \t        1e-06 \n",
      " alpha2 \t        3e-05 \n",
      " h0 \t      0.00023 \n",
      " Nx \t            0 \n",
      " Ny \t            0 \n",
      " Nxy \t            0 \n",
      " Mx \t            0 \n",
      " My \t            0 \n",
      " Mxy \t            0 \n",
      " dT \t            0Theta 45 -45 -45  45</current>\n",
      "            <about>\n",
      "                <label>Inputs</label>\n",
      "            </about>\n",
      "        </string>\n",
      "        <curve id=\"sigX\">\n",
      "            <component>\n",
      "                <xy>           0            -2\n",
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      "           0            -1\n",
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      "           0             1\n",
      "           0             2\n",
      "</xy>\n",
      "            </component>\n",
      "            <about>\n",
      "                <group>Stress Through Thickness, Laminate Coordinate System</group>\n",
      "                <label>sigma_{x}</label>\n",
      "            </about>\n",
      "        </curve>\n",
      "        <curve id=\"sigY\">\n",
      "            <component>\n",
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      "                <group>Stress Through Thickness, Laminate Coordinate System</group>\n",
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      "            </about>\n",
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      "        <curve id=\"tauXY\">\n",
      "            <component>\n",
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      "</xy>\n",
      "            </component>\n",
      "            <about>\n",
      "                <group>Stress Through Thickness, Laminate Coordinate System</group>\n",
      "                <label>tau_{xy}</label>\n",
      "            </about>\n",
      "            <xaxis>\n",
      "                <label>Stess</label>\n",
      "                <units>Pa</units>\n",
      "            </xaxis>\n",
      "            <yaxis>\n",
      "                <label>Through Thickness Location z/h0</label>\n",
      "                <units>-</units>\n",
      "            </yaxis>\n",
      "        </curve>\n",
      "        <curve id=\"sig1\">\n",
      "            <component>\n",
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      "                <group>Stress Through Thickness, Material Coordinate System</group>\n",
      "                <label>sigma_{1}</label>\n",
      "            </about>\n",
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      "        <curve id=\"sig2\">\n",
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      "           0             2\n",
      "</xy>\n",
      "            </component>\n",
      "            <about>\n",
      "                <group>Stress Through Thickness, Material Coordinate System</group>\n",
      "                <label>sigma_{2}</label>\n",
      "            </about>\n",
      "        </curve>\n",
      "        <curve id=\"tau12\">\n",
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      "            <about>\n",
      "                <group>Stress Through Thickness, Material Coordinate System</group>\n",
      "                <label>tau_{12}</label>\n",
      "            </about>\n",
      "            <xaxis>\n",
      "                <label>Stess</label>\n",
      "                <units>Pa</units>\n",
      "            </xaxis>\n",
      "            <yaxis>\n",
      "                <label>Through Thickness Location z/h0</label>\n",
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      "</xy>\n",
      "            </component>\n",
      "            <about>\n",
      "                <group>Strain Through Thickness, Laminate Coordinate System</group>\n",
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      "            </about>\n",
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      "            <about>\n",
      "                <group>Strain Through Thickness, Laminate Coordinate System</group>\n",
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      "            <about>\n",
      "                <group>Strain Through Thickness, Laminate Coordinate System</group>\n",
      "                <label>gamma_{xy}</label>\n",
      "            </about>\n",
      "            <xaxis>\n",
      "                <label>Strain</label>\n",
      "                <units>-</units>\n",
      "            </xaxis>\n",
      "            <yaxis>\n",
      "                <label>Through Thickness Location z/h0</label>\n",
      "                <units>-</units>\n",
      "            </yaxis>\n",
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      "        <curve id=\"eps1\">\n",
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      "           0             0\n",
      "           0             1\n",
      "           0             1\n",
      "           0             2\n",
      "</xy>\n",
      "            </component>\n",
      "            <about>\n",
      "                <group>Strain Through Thickness, Material Coordinate System</group>\n",
      "                <label>gamma_{12}</label>\n",
      "            </about>\n",
      "            <xaxis>\n",
      "                <label>Strain</label>\n",
      "                <units>-</units>\n",
      "            </xaxis>\n",
      "            <yaxis>\n",
      "                <label>Through Thickness Location z/h0</label>\n",
      "                <units>-</units>\n",
      "            </yaxis>\n",
      "        </curve>\n",
      "        <string id=\"Laminate\">\n",
      "            <about>\n",
      "                <label>Effective Laminate Properties</label>\n",
      "            </about>\n",
      "            <current>Ex =        23.44 \n",
      " Ey =        23.44 \n",
      " nuxy =            1 \n",
      " Gxy =  3.50214e+10 \n",
      " alphax =  4.01134e-06 \n",
      " alphay =  4.01137e-06 \n",
      " alphaxy =            0</current>\n",
      "        </string>\n",
      "        <number id=\"Ex\">\n",
      "            <current>       23.44 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Longitudinal Modulus</label>\n",
      "            </about>\n",
      "            <units>Pa</units>\n",
      "        </number>\n",
      "        <number id=\"Ey\">\n",
      "            <current>       23.44 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Transverse Modulus</label>\n",
      "            </about>\n",
      "            <units>Pa</units>\n",
      "        </number>\n",
      "        <number id=\"Gxy\">\n",
      "            <current> 3.50214e+10 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Shear Modulus</label>\n",
      "            </about>\n",
      "            <units>Pa</units>\n",
      "        </number>\n",
      "        <number id=\"nu\">\n",
      "            <current>           1 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Poisson ratio</label>\n",
      "            </about>\n",
      "        </number>\n",
      "        <number id=\"alphax\">\n",
      "            <current> 4.01134e-06 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Thermal Expansion (x)</label>\n",
      "            </about>\n",
      "        </number>\n",
      "        <number id=\"alphay\">\n",
      "            <current> 4.01137e-06 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Thermal Expansion (y)</label>\n",
      "            </about>\n",
      "        </number>\n",
      "        <number id=\"alphaxy\">\n",
      "            <current>           0 \n",
      "</current>\n",
      "            <about>\n",
      "                <label>Thermal Expansion (xy)</label>\n",
      "            </about>\n",
      "        </number>\n",
      "        <time>Fri Jul 20 08:56:09 AM EDT 2018</time>\n",
      "        <status>ok</status>\n",
      "        <user>dcelbert</user>\n",
      "        <host/>\n",
      "        <session>1336474</session>\n",
      "        <filename>/home/nanohub/dcelbert/data/results/1336474/run153209136982538.xml</filename>\n",
      "        <version>1.7</version>\n",
      "    </output>\n",
      "</run>\n",
      "\n",
      "\n"
     ]
    }
   ],
   "source": [
    "print run_results"
   ]
  },
  {
   "cell_type": "code",
   "execution_count": null,
   "metadata": {},
   "outputs": [],
   "source": []
  }
 ],
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