From aa03b369272ec6d5b47600b72f8c673848f0860a Mon Sep 17 00:00:00 2001 From: Joshua Drake 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