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Anson Biggs
2021-04-01 23:25:04 -07:00
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_posts/2021-04-01-air-propulsion-simulation/air-propulsion-simulation.Rmd
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@@ -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

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_posts/2021-04-01-air-propulsion-simulation/air-propulsion-simulation.html
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@@ -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."/>
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<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"/>
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@@ -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>
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</div>
@@ -1574,6 +1582,8 @@ Show code
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<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>