added citations

_posts/2021-04-01-air-propulsion-simulation/air-propulsion-simulation.Rmd

@@ -15,6 +15,7 @@ output:
 categories:
   - Julia
   - Capstone
+bibliography: ../../citations.bib
 ---
 
 Boilerplate intro about why all of this was done
@@ -37,7 +38,7 @@ using Measurements
 using Measurements: value, uncertainty
 ```
 
-This code is just the setup the setup, using values scraped from various parts of the world wide web. 
+This code is just the setup, using values scraped from various parts of the world wide web. 
 
 ```{julia}
 # Tank https://www.amazon.com/Empire-Paintball-BASICS-Pressure-Compressed/dp/B07B6M48SR/
@@ -64,7 +65,7 @@ This is the actual simulation. Maybe throw some references in and explain some e
 The rocket equation is pretty sick:
 
 $$T = \dot{m} \cdot v_\text{Exit} + A_\text{Nozzle} \cdot (P - P_\text{Ambient}) $$
-And thats about all you need to get to the moon. 
+And thats about all you need to get to the moon[@curtis_orbital]. 
 
 ```{julia}
 let

_posts/2021-04-01-air-propulsion-simulation/air-propulsion-simulation.html

@@ -108,10 +108,12 @@ code span.wa { color: #5e5e5e; font-style: italic; } /* Warning */
   <meta property="twitter:description" content="Simulating the performace of an air propulsion system as an alternative to solid rocket motors."/>
 
   <!--/radix_placeholder_meta_tags-->
+  
+  <meta name="citation_reference" content="citation_title=Orbital mechanics for engineering students;citation_publication_date=2020;citation_publisher=Butterworth-Heinemann Publications;citation_author=Howard D Curtis"/>
   <!--radix_placeholder_rmarkdown_metadata-->
 
   <script type="text/json" id="radix-rmarkdown-metadata">
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+  {"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["title","description","author","repository_url","date","fig_width","fig_align","output","categories","bibliography"]}},"value":[{"type":"character","attributes":{},"value":["Air Propulsion Simulation"]},{"type":"character","attributes":{},"value":["Simulating the performace of an air propulsion system as an alternative to solid rocket motors. \n"]},{"type":"list","attributes":{},"value":[{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["name","url"]}},"value":[{"type":"character","attributes":{},"value":["Anson Biggs"]},{"type":"character","attributes":{},"value":["https://ansonbiggs.com"]}]}]},{"type":"character","attributes":{},"value":["https://gitlab.com/lander-team/air-prop-simulation"]},{"type":"character","attributes":{},"value":["04-01-2021"]},{"type":"integer","attributes":{},"value":[6]},{"type":"character","attributes":{},"value":["center"]},{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["distill::distill_article"]}},"value":[{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["self_contained"]}},"value":[{"type":"logical","attributes":{},"value":[false]}]}]},{"type":"character","attributes":{},"value":["Julia","Capstone"]},{"type":"character","attributes":{},"value":["../../citations.bib"]}]}
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   <!--/radix_placeholder_rmarkdown_metadata-->
   
@@ -1498,7 +1500,7 @@ Show code
 <span id="cb1-8"><a href="#cb1-8" aria-hidden="true" tabindex="-1"></a><span class="kw">using</span> Measurements<span class="op">:</span> value<span class="op">,</span> uncertainty</span></code></pre></div>
 </details>
 </div>
-<p>This code is just the setup the setup, using values scraped from various parts of the world wide web.</p>
+<p>This code is just the setup, using values scraped from various parts of the world wide web.</p>
 <div class="layout-chunk" data-layout="l-body">
 <div class="sourceCode" id="cb2"><pre class="sourceCode julia"><code class="sourceCode julia"><span id="cb2-1"><a href="#cb2-1" aria-hidden="true" tabindex="-1"></a><span class="co"># Tank https://www.amazon.com/Empire-Paintball-BASICS-Pressure-Compressed/dp/B07B6M48SR/</span></span>
 <span id="cb2-2"><a href="#cb2-2" aria-hidden="true" tabindex="-1"></a>V <span class="op">=</span> (<span class="fl">85</span> ± <span class="fl">5</span>)u<span class="st">&quot;inch^3&quot;</span></span>
@@ -1520,7 +1522,7 @@ Show code
 </div>
 <p>This is the actual simulation. Maybe throw some references in and explain some equations.</p>
 <p>The rocket equation is pretty sick:</p>
-<p><span class="math display">\[T = \dot{m} \cdot v_\text{Exit} + A_\text{Nozzle} \cdot (P - P_\text{Ambient}) \]</span> And thats about all you need to get to the moon.</p>
+<p><span class="math display">\[T = \dot{m} \cdot v_\text{Exit} + A_\text{Nozzle} \cdot (P - P_\text{Ambient}) \]</span> And thats about all you need to get to the moon<span class="citation" data-cites="curtis_orbital">(<a href="#ref-curtis_orbital" role="doc-biblioref">Curtis 2020</a>)</span>.</p>
 <div class="layout-chunk" data-layout="l-body">
 <div class="sourceCode" id="cb3"><pre class="sourceCode julia"><code class="sourceCode julia"><span id="cb3-1"><a href="#cb3-1" aria-hidden="true" tabindex="-1"></a><span class="kw">let</span></span>
 <span id="cb3-2"><a href="#cb3-2" aria-hidden="true" tabindex="-1"></a>t <span class="op">=</span> <span class="fl">0.0</span>u<span class="st">&quot;s&quot;</span></span>
@@ -1552,7 +1554,13 @@ Show code
 <div class="layout-chunk" data-layout="l-body">
 <p><img src="air-propulsion-simulation_files/figure-html5/unnamed-chunk-4-J1.png" width="350" /></p>
 </div>
+<p>Big conclusion about things.</p>
 <div class="sourceCode" id="cb4"><pre class="sourceCode r distill-force-highlighting-css"><code class="sourceCode r"></code></pre></div>
+<div id="refs" class="references csl-bib-body hanging-indent" role="doc-bibliography">
+<div id="ref-curtis_orbital" class="csl-entry" role="doc-biblioentry">
+Curtis, Howard D. 2020. <em>Orbital Mechanics for Engineering Students</em>. Fourth edition. Butterworth-Heinemann Publications.
+</div>
+</div>
 <!--radix_placeholder_article_footer-->
 <!--/radix_placeholder_article_footer-->
 </div>
@@ -1574,6 +1582,8 @@ Show code
 <!--/radix_placeholder_site_after_body-->
 <!--radix_placeholder_appendices-->
 <div class="appendix-bottom">
+<h3 id="references">References</h3>
+<div id="references-listing"></div>
 <h3 id="updates-and-corrections">Corrections</h3>
 <p>If you see mistakes or want to suggest changes, please <a href="https://gitlab.com/lander-team/air-prop-simulation">create an issue</a> on the source repository.</p>
 </div>

_site.yml

@@ -9,4 +9,6 @@ navbar:
       href: index.html
     - text: "About"
       href: about.html
+    - text: "Resume"
+      href: https://ansonbiggs.com
 output: distill::distill_article

citations.bib

@@ -0,0 +1,23 @@
+
+@book{shackelford_introduction_2015,
+	address = {Boston},
+	edition = {Eighth edition},
+	title = {Introduction to materials science for engineers},
+	isbn = {9780133826654},
+	publisher = {Pearson},
+	author = {Shackelford, James F.},
+	year = {2015},
+	keywords = {Materials},
+}
+
+@book{curtis_orbital,
+	title = {Orbital mechanics for engineering students},
+	isbn = {9780128240250 9780323853453 9780081021330},
+	language = {English},
+	author = {Curtis, Howard D},
+	year = {2020},
+	note = {OCLC: 1235349370},
+	publisher = {Butterworth-Heinemann Publications},
+	edition = {Fourth edition}
+
+}

docs/about.html

@@ -2067,6 +2067,7 @@ code span.wa { color: #5e5e5e; font-style: italic; } /* Warning */
 <div class="nav-right">
 <a href="index.html">Home</a>
 <a href="about.html">About</a>
+<a href="https://ansonbiggs.com">Resume</a>
 <a href="javascript:void(0);" class="nav-toggle">&#9776;</a>
 </div>
 </nav>

docs/index.html

@@ -2064,6 +2064,7 @@ code span.wa { color: #5e5e5e; font-style: italic; } /* Warning */
 <div class="nav-right">
 <a href="index.html">Home</a>
 <a href="about.html">About</a>
+<a href="https://ansonbiggs.com">Resume</a>
 <a href="javascript:void(0);" class="nav-toggle">&#9776;</a>
 </div>
 </nav>
@@ -2206,24 +2207,6 @@ function init_posts_list() {
 <div class="posts-container posts-with-sidebar posts-apply-limit l-screen-inset">
 <div class="posts-list">
 <h1 class="posts-list-caption" data-caption="Anson&#39;s Projects">Anson's Projects</h1>
-<a href="posts/welcome/" class="post-preview">
-<script class="post-metadata" type="text/json">{"categories":[]}</script>
-<div class="metadata">
-<div class="publishedDate">April 1, 2021</div>
-<div class="dt-authors">
-<div class="dt-author">Nora Jones</div>
-</div>
-</div>
-<div class="thumbnail">
-<img/>
-</div>
-<div class="description">
-<h2>Welcome to Anson's Projects</h2>
-<div class="dt-tags"></div>
-<p>Welcome to our new blog, Anson's Projects. We hope you enjoy 
-reading what we have to say!</p>
-</div>
-</a>
 <a href="posts/2021-04-01-air-propulsion-simulation/" class="post-preview">
 <script class="post-metadata" type="text/json">{"categories":["Julia","Capstone"]}</script>
 <div class="metadata">
@@ -2244,6 +2227,24 @@ reading what we have to say!</p>
 <p>Simulating the performace of an air propulsion system as an alternative to solid rocket motors.</p>
 </div>
 </a>
+<a href="posts/welcome/" class="post-preview">
+<script class="post-metadata" type="text/json">{"categories":[]}</script>
+<div class="metadata">
+<div class="publishedDate">April 1, 2021</div>
+<div class="dt-authors">
+<div class="dt-author">Nora Jones</div>
+</div>
+</div>
+<div class="thumbnail">
+<img/>
+</div>
+<div class="description">
+<h2>Welcome to Anson's Projects</h2>
+<div class="dt-tags"></div>
+<p>Welcome to our new blog, Anson's Projects. We hope you enjoy 
+reading what we have to say!</p>
+</div>
+</a>
 </div>
 <div class="posts-sidebar">
 <div class="sidebar-section categories">

docs/posts/2021-04-01-air-propulsion-simulation/index.html

@@ -109,10 +109,12 @@ code span.wa { color: #5e5e5e; font-style: italic; } /* Warning */
 <meta property="twitter:description" content="Simulating the performace of an air propulsion system as an alternative to solid rocket motors."/>
 
 <!--/radix_placeholder_meta_tags-->
+  
+  <meta name="citation_reference" content="citation_title=Orbital mechanics for engineering students;citation_publication_date=2020;citation_publisher=Butterworth-Heinemann Publications;citation_author=Howard D Curtis"/>
   <!--radix_placeholder_rmarkdown_metadata-->
 
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+{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["title","description","author","repository_url","date","fig_width","fig_align","output","categories","bibliography"]}},"value":[{"type":"character","attributes":{},"value":["Air Propulsion Simulation"]},{"type":"character","attributes":{},"value":["Simulating the performace of an air propulsion system as an alternative to solid rocket motors."]},{"type":"list","attributes":{},"value":[{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["name","url"]}},"value":[{"type":"character","attributes":{},"value":["Anson Biggs"]},{"type":"character","attributes":{},"value":["https://ansonbiggs.com"]}]}]},{"type":"character","attributes":{},"value":["https://gitlab.com/lander-team/air-prop-simulation"]},{"type":"character","attributes":{},"value":["04-01-2021"]},{"type":"integer","attributes":{},"value":[6]},{"type":"character","attributes":{},"value":["center"]},{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["distill::distill_article"]}},"value":[{"type":"list","attributes":{"names":{"type":"character","attributes":{},"value":["self_contained"]}},"value":[{"type":"logical","attributes":{},"value":[false]}]}]},{"type":"character","attributes":{},"value":["Julia","Capstone"]},{"type":"character","attributes":{},"value":["../../citations.bib"]}]}
 </script>
 <!--/radix_placeholder_rmarkdown_metadata-->
   
@@ -2076,6 +2078,7 @@ document.addEventListener('DOMContentLoaded', function() {
 <div class="nav-right">
 <a href="../../index.html">Home</a>
 <a href="../../about.html">About</a>
+<a href="https://ansonbiggs.com">Resume</a>
 <a href="javascript:void(0);" class="nav-toggle">&#9776;</a>
 </div>
 </nav>
@@ -2118,7 +2121,7 @@ Show code
 <span id="cb1-8"><a href="#cb1-8" aria-hidden="true" tabindex="-1"></a><span class="kw">using</span> Measurements<span class="op">:</span> value<span class="op">,</span> uncertainty</span></code></pre></div>
 </details>
 </div>
-<p>This code is just the setup the setup, using values scraped from various parts of the world wide web.</p>
+<p>This code is just the setup, using values scraped from various parts of the world wide web.</p>
 <div class="layout-chunk" data-layout="l-body">
 <div class="sourceCode" id="cb2"><pre class="sourceCode julia"><code class="sourceCode julia"><span id="cb2-1"><a href="#cb2-1" aria-hidden="true" tabindex="-1"></a><span class="co"># Tank https://www.amazon.com/Empire-Paintball-BASICS-Pressure-Compressed/dp/B07B6M48SR/</span></span>
 <span id="cb2-2"><a href="#cb2-2" aria-hidden="true" tabindex="-1"></a>V <span class="op">=</span> (<span class="fl">85</span> ± <span class="fl">5</span>)u<span class="st">&quot;inch^3&quot;</span></span>
@@ -2140,7 +2143,7 @@ Show code
 </div>
 <p>This is the actual simulation. Maybe throw some references in and explain some equations.</p>
 <p>The rocket equation is pretty sick:</p>
-<p><span class="math display">\[T = \dot{m} \cdot v_\text{Exit} + A_\text{Nozzle} \cdot (P - P_\text{Ambient}) \]</span> And thats about all you need to get to the moon.</p>
+<p><span class="math display">\[T = \dot{m} \cdot v_\text{Exit} + A_\text{Nozzle} \cdot (P - P_\text{Ambient}) \]</span> And thats about all you need to get to the moon<span class="citation" data-cites="curtis_orbital">(<a href="#ref-curtis_orbital" role="doc-biblioref">Curtis 2020</a>)</span>.</p>
 <div class="layout-chunk" data-layout="l-body">
 <div class="sourceCode" id="cb3"><pre class="sourceCode julia"><code class="sourceCode julia"><span id="cb3-1"><a href="#cb3-1" aria-hidden="true" tabindex="-1"></a><span class="kw">let</span></span>
 <span id="cb3-2"><a href="#cb3-2" aria-hidden="true" tabindex="-1"></a>t <span class="op">=</span> <span class="fl">0.0</span>u<span class="st">&quot;s&quot;</span></span>
@@ -2172,7 +2175,13 @@ Show code
 <div class="layout-chunk" data-layout="l-body">
 <p><img src="air-propulsion-simulation_files/figure-html5/unnamed-chunk-4-J1.png" width="350" /></p>
 </div>
+<p>Big conclusion about things.</p>
 <div class="sourceCode" id="cb4"><pre class="sourceCode r distill-force-highlighting-css"><code class="sourceCode r"></code></pre></div>
+<div id="refs" class="references csl-bib-body hanging-indent" role="doc-bibliography">
+<div id="ref-curtis_orbital" class="csl-entry" role="doc-biblioentry">
+Curtis, Howard D. 2020. <em>Orbital Mechanics for Engineering Students</em>. Fourth edition. Butterworth-Heinemann Publications.
+</div>
+</div>
 <!--radix_placeholder_article_footer-->
 <!--/radix_placeholder_article_footer-->
 </div>
@@ -2194,6 +2203,8 @@ Show code
 <!--/radix_placeholder_site_after_body-->
 <!--radix_placeholder_appendices-->
 <div class="appendix-bottom">
+  <h3 id="references">References</h3>
+  <div id="references-listing"></div>
   <h3 id="updates-and-corrections">Corrections</h3>
   <p>If you see mistakes or want to suggest changes, please <a href="https://gitlab.com/lander-team/air-prop-simulation">create an issue</a> on the source repository.</p>
 </div>

docs/posts/posts.json

@@ -1,4 +1,24 @@
 [
+  {
+    "path": "posts/2021-04-01-air-propulsion-simulation/",
+    "title": "Air Propulsion Simulation",
+    "description": "Simulating the performace of an air propulsion system as an alternative to solid rocket motors.",
+    "author": [
+      {
+        "name": "Anson Biggs",
+        "url": "https://ansonbiggs.com"
+      }
+    ],
+    "date": "2021-04-01",
+    "categories": [
+      "Julia",
+      "Capstone"
+    ],
+    "contents": "\nBoilerplate intro about why all of this was done\n\n\nShow code\nusing Plots\nplotly()\ntheme(:ggplot2); # In true R spirit\n\nusing Unitful\nusing DataFrames\nusing Measurements\nusing Measurements: value, uncertainty\n\nThis code is just the setup, using values scraped from various parts of the world wide web.\n\n# Tank https://www.amazon.com/Empire-Paintball-BASICS-Pressure-Compressed/dp/B07B6M48SR/\nV = (85 ± 5)u\"inch^3\"\nP0 = (4200.0 ± 300)u\"psi\"\nWtank = (2.3 ± 0.2)u\"lb\"\nPmax = (250 ± 50)u\"psi\" # Max Pressure that can come out the nozzle\n\nWsolenoid = 1.5u\"kg\"\n\n# Params\nd_nozzle = ((1 // 18) ± 0.001)u\"inch\"\na_nozzle = (pi / 4) * d_nozzle^2\n\n# Universal Stuff\nP_amb = (1 ± 0.2)u\"atm\"\nγ = 1.4 ± 0.05\nR = 287.05u\"J/(kg * K)\"\nT = (300 ± 20)u\"K\"\n\nThis is the actual simulation. Maybe throw some references in and explain some equations.\nThe rocket equation is pretty sick:\n\\[T = \\dot{m} \\cdot v_\\text{Exit} + A_\\text{Nozzle} \\cdot (P - P_\\text{Ambient}) \\] And thats about all you need to get to the moon(Curtis 2020).\n\nlet\nt = 0.0u\"s\"\nP = P0 |> u\"Pa\"\nM = V * (P / (R * T)) |> u\"kg\"\nts = 1u\"ms\"\nglobal df = DataFrame(Thrust=(0 ± 0)u\"N\", Pressure=P0, Time=0.0u\"s\", Mass=M)\n  while M > 0.005u\"kg\"\n      # while t < 30u\"s\"\n      # Calculate what is leaving tank\n      P = minimum([P, Pmax])\n      ve = sqrt((2 * γ / (γ - 1)) * R * T * (1 - P_amb / P)^((γ - 1) / γ)) |> u\"m/s\"\n      ρ = P / (R * T) |> u\"kg/m^3\"\n      ṁ = ρ * a_nozzle * ve |> u\"kg/s\"\n  \n      Thrust = ṁ * ve + a_nozzle * (P - P_amb) |> u\"N\"\n  \n      # Calculate what is still in the tank\n      M = M - ṁ * ts |> u\"kg\"\n      P = (M * R * T) / V |> u\"Pa\"\n      t = t + ts\n  \n      df_step = DataFrame(Thrust=Thrust, Pressure=P, Time=t, Mass=M)\n      append!(df, df_step)\n  end\nend\n\nHeres the results plotted. Notice the massive error once the tank starts running low.\n\n\n\nBig conclusion about things.\n\n\n\nCurtis, Howard D. 2020. Orbital Mechanics for Engineering Students. Fourth edition. Butterworth-Heinemann Publications.\n\n\n\n\n",
+    "preview": "posts/2021-04-01-air-propulsion-simulation/air-propulsion-simulation_files/figure-html5/unnamed-chunk-4-J1.png",
+    "last_modified": "2021-04-01T23:23:11-07:00",
+    "input_file": {}
+  },
   {
     "path": "posts/welcome/",
     "title": "Welcome to Anson's Projects",
@@ -15,25 +35,5 @@
     "preview": {},
     "last_modified": "2021-04-01T20:38:44-07:00",
     "input_file": {}
-  },
-  {
-    "path": "posts/2021-04-01-air-propulsion-simulation/",
-    "title": "Air Propulsion Simulation",
-    "description": "Simulating the performace of an air propulsion system as an alternative to solid rocket motors.",
-    "author": [
-      {
-        "name": "Anson Biggs",
-        "url": "https://ansonbiggs.com"
-      }
-    ],
-    "date": "2021-04-01",
-    "categories": [
-      "Julia",
-      "Capstone"
-    ],
-    "contents": "\nBoilerplate intro about why all of this was done\n\n\nShow code\nusing Plots\nplotly()\ntheme(:ggplot2); # In true R spirit\n\nusing Unitful\nusing DataFrames\nusing Measurements\nusing Measurements: value, uncertainty\n\nThis code is just the setup the setup, using values scraped from various parts of the world wide web.\n\n# Tank https://www.amazon.com/Empire-Paintball-BASICS-Pressure-Compressed/dp/B07B6M48SR/\nV = (85 ± 5)u\"inch^3\"\nP0 = (4200.0 ± 300)u\"psi\"\nWtank = (2.3 ± 0.2)u\"lb\"\nPmax = (250 ± 50)u\"psi\" # Max Pressure that can come out the nozzle\n\nWsolenoid = 1.5u\"kg\"\n\n# Params\nd_nozzle = ((1 // 18) ± 0.001)u\"inch\"\na_nozzle = (pi / 4) * d_nozzle^2\n\n# Universal Stuff\nP_amb = (1 ± 0.2)u\"atm\"\nγ = 1.4 ± 0.05\nR = 287.05u\"J/(kg * K)\"\nT = (300 ± 20)u\"K\"\n\nThis is the actual simulation. Maybe throw some references in and explain some equations.\nThe rocket equation is pretty sick:\n\\[T = \\dot{m} \\cdot v_\\text{Exit} + A_\\text{Nozzle} \\cdot (P - P_\\text{Ambient}) \\] And thats about all you need to get to the moon.\n\nlet\nt = 0.0u\"s\"\nP = P0 |> u\"Pa\"\nM = V * (P / (R * T)) |> u\"kg\"\nts = 1u\"ms\"\nglobal df = DataFrame(Thrust=(0 ± 0)u\"N\", Pressure=P0, Time=0.0u\"s\", Mass=M)\n  while M > 0.005u\"kg\"\n      # while t < 30u\"s\"\n      # Calculate what is leaving tank\n      P = minimum([P, Pmax])\n      ve = sqrt((2 * γ / (γ - 1)) * R * T * (1 - P_amb / P)^((γ - 1) / γ)) |> u\"m/s\"\n      ρ = P / (R * T) |> u\"kg/m^3\"\n      ṁ = ρ * a_nozzle * ve |> u\"kg/s\"\n  \n      Thrust = ṁ * ve + a_nozzle * (P - P_amb) |> u\"N\"\n  \n      # Calculate what is still in the tank\n      M = M - ṁ * ts |> u\"kg\"\n      P = (M * R * T) / V |> u\"Pa\"\n      t = t + ts\n  \n      df_step = DataFrame(Thrust=Thrust, Pressure=P, Time=t, Mass=M)\n      append!(df, df_step)\n  end\nend\n\nHeres the results plotted. Notice the massive error once the tank starts running low.\n\n\n\n\n\n\n",
-    "preview": "posts/2021-04-01-air-propulsion-simulation/air-propulsion-simulation_files/figure-html5/unnamed-chunk-4-J1.png",
-    "last_modified": "2021-04-01T22:49:43-07:00",
-    "input_file": "air-propulsion-simulation.utf8.md"
   }
 ]

docs/posts/welcome/index.html

@@ -2076,6 +2076,7 @@ document.addEventListener('DOMContentLoaded', function() {
 <div class="nav-right">
 <a href="../../index.html">Home</a>
 <a href="../../about.html">About</a>
+<a href="https://ansonbiggs.com">Resume</a>
 <a href="javascript:void(0);" class="nav-toggle">&#9776;</a>
 </div>
 </nav>

docs/search.json

@@ -6,14 +6,14 @@
       "description": "Some additional details about the blog",
       "author": [],
       "contents": "\n\n\n\n",
-      "last_modified": "2021-04-01T20:38:45-07:00"
+      "last_modified": "2021-04-01T23:24:45-07:00"
     },
     {
       "path": "index.html",
       "title": "Anson's Projects",
       "author": [],
       "contents": "\n\n\n\n",
-      "last_modified": "2021-04-01T20:40:59-07:00"
+      "last_modified": "2021-04-01T23:24:45-07:00"
     }
   ],
   "collections": ["posts/posts.json"]