Added a design_evaluator dummy config for propulsion design. Needs to be...

Added a design_evaluator dummy config for propulsion design. Needs to be adapted to specific propulsion_design values later

design_evaluator/design_evaluator_conf_propulsion_design.xml

+<config_file Name="design_evaluator_conf.xml">
+    <program_settings Desc="program settings">
+        <aircraft_design ID="0" Desc="reference draft"> 
+            <name Desc="Name" Unit="-" Default="">CSR-02 Reference Design</name>
+            <file_name Desc="Name" Unit="-" Default="">newFormat-CSMR-2020.xml</file_name>
+            <design_directory Desc="Path" Unit="-" Default="">./test-upstream-files/</design_directory>
+        </aircraft_design>
+        <aircraft_design ID="1">
+            <name Desc="Name" Unit="-" Default="">CSR nr1</name>
+            <file_name Desc="Name" Unit="-" Default="">newFormat-CSMR-2020_0.xml</file_name>
+            <design_directory Desc="Path" Unit="-" Default="">./projects/</design_directory>
+        </aircraft_design>
+        <aircraft_design ID="2">
+            <name Desc="Name" Unit="-" Default="">CSR nr2</name>
+            <file_name Desc="Name" Unit="-" Default="">newFormat-CSMR-2020_1.xml</file_name>
+            <design_directory Desc="Path" Unit="-" Default="">./projects/</design_directory>
+        </aircraft_design>
+        <aircraft_design ID="3">
+            <name Desc="Name" Unit="-" Default="">CSR nr3</name>
+            <file_name Desc="Name" Unit="-" Default="">newFormat-CSMR-2020_2.xml</file_name>
+            <design_directory Desc="Path" Unit="-" Default="">./projects/</design_directory>
+        </aircraft_design>
+    </program_settings>
+    <parameters Desc="parameters to be compared">
+            <something>
+                <sub_path ID="0" Name="MTOM">analysis/masses_cg_inertia/maximum_takeoff_mass/mass_properties/mass/value</sub_path>
+            </something>
+            <sub_path ID="1" Name="Moment of Inertia">analysis/masses_cg_inertia/maximum_takeoff_mass/mass_properties/inertia/j_xx/value</sub_path>
+            <sub_path ID="2" Name="OME">analysis/masses_cg_inertia/operating_mass_empty/mass_properties/mass/value</sub_path>
+            <sub_path ID="3" Name="Some Name">requirements_and_specifications/design_specification/propulsion/propulsor@1/energy_carrier_ID/value</sub_path>
+            <sub_path ID="4" Name="Another Name">requirements_and_specifications/design_specification/propulsion/propulsor@123/energy_carrier_ID/value</sub_path>
+        </parameters>
+</config_file>