From aa03b369272ec6d5b47600b72f8c673848f0860a Mon Sep 17 00:00:00 2001
From: Joshua Drake <joshua.ellis.drake@gmail.com>
Date: Fri, 1 Nov 2024 17:02:39 -0500
Subject: Commit ahead of weekly meeting.

---
 background.tex | 3 +++
 1 file changed, 3 insertions(+)

(limited to 'background.tex')

diff --git a/background.tex b/background.tex
index 8c26e4d..0bfe584 100644
--- a/background.tex
+++ b/background.tex
@@ -41,6 +41,9 @@ Turboshaft style engines are most often used in helicopters, and are characteriz
 \end{figure}
 \section{Generator Theory}
 \section{Battery Theory}
+\begin{equation}\label{battC}
+	I_{Battery}=\frac{V_{Battery}-V_{Supply}}{R_{Battery}}
+\end{equation}
 \section{Turboelectric Theory}
 NASA defines turboelectric systems as being at the least a turboshaft coupled to an electric generator, which power electric motors which then drive propellers. This configuration can be further categorized in accordance with whether the turbine engine drives a load directly.
 These systems, refered to as "Partial Turbo Electric" \cite{nasa_prop_overview}, employ the use of either turbofans or turboprops in addition to being coupled to electric generators.
-- 
cgit v1.2.3

