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author | Joshua Drake <joshua.ellis.drake@gmail.com> | 2024-11-01 17:02:39 -0500 |
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committer | Joshua Drake <joshua.ellis.drake@gmail.com> | 2024-11-01 17:02:39 -0500 |
commit | aa03b369272ec6d5b47600b72f8c673848f0860a (patch) | |
tree | 27009c1b62794961791ad8e6283497d92727af3a /background.tex | |
parent | 01515d09923f66fff330f08316c53c58f7adaaef (diff) |
Commit ahead of weekly meeting.
Diffstat (limited to 'background.tex')
-rw-r--r-- | background.tex | 3 |
1 files changed, 3 insertions, 0 deletions
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. |