getting_started.md:

- Updated equations
- Fixed some formatting

docs/documentation/sizing/tank_design/getting_started.md

@@ -47,9 +47,9 @@ To single execute the _tank\_design_ module, we need an _acXML_ file that alread
 
 <sup>*</sup> The _tank\_design_ execution is also possible without mission analysis data. Alternatively, the following assumption is used to calculate the mission fuel amount:
 
-$
+$$
     m_{fuel} = n_{PAX} \cdot R \cdot \frac{E}{100 \text{ km}}
-$
+$$
 
 In which
 
@@ -80,6 +80,7 @@ The desired tank configuration is defined by the user in the aircraft exchange f
 
 ### The ID `tank_element`
 Each tank is configured in the _acXML_ as one element (ID element) with the following parameters:
+
 - `energy_carrier_ID`: ID of energy carrier to obtain which fuel is to be stored in the tanks.
 - `location`: Aircraft component where the tank is located (valid options depend on the energy carrier).
 - `position`: Position at the desired location (valid options depend on location and energy carrier).
@@ -107,6 +108,7 @@ For aircraft configurations with a kinked wing, the "wing tank configuration" co
 |  7  | Fuselage              | Center      | Also referred to as 'additional center tank'. |
 
 For example, to define a valid combination for the wing center tank, set the following parameters for the ID element `ID="0"`:
+
 - `energy_carrier_ID` to `0` (it is assumed that `0` equals kerosene)
 - `location` to `wing`
 - `position` to `center`
@@ -126,6 +128,7 @@ The following table provides an overview on possible tank configurations. As can
 | Wing       | Fuselage - Center             |               -               | wing_with_additional_center_tank         |
 | Wing       | Horizontal stabilizer - Total | Fuselage - Center             | wing_with_additional_center_and_trim_tank|
 | Wing       | Fuselage - Center             | Horizontal stabilizer - Total | wing_with_additional_center_and_trim_tank|
+
 Note: "Wing" always refers to either the combinations 1 to 5 of the table in the previous section ("wing tank configuration").
 
 #### Possible tank configurations: Aircraft with singe trapezoidal wing
@@ -138,6 +141,7 @@ The following table provides an overview on possible tank configurations. As can
 | Wing       | Fuselage - Center             |               -               | wing_with_additional_center_tank         |
 | Wing       | Horizontal stabilizer - Total | Fuselage - Center             | wing_with_additional_center_and_trim_tank|
 | Wing       | Fuselage - Center             | Horizontal stabilizer - Total | wing_with_additional_center_and_trim_tank|
+
 Note: "Wing" always refers to the combinations 1, 2, and 4 of the table in the previous section ("wing tank configuration").
 
 #### Example: Minimum tank configuration
@@ -258,6 +262,7 @@ tbd. :construction:
 The _configXML_ is structured into two blocks: the control and program settings.
 
 The control settings are standardized in UNICADO and will not be described in detail here. But to get started, you have to change at least
+
 - the `aircraft_exchange_file_name` and `aircraft_exchange_file_directory` to your respective settings,
 - the `console_output` at least to `mode_1`, and
 - the `plot_output` to false (or define `inkscape_path` and `gnuplot_path`).