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Created with Raphaël 2.2.09Jan8763220Dec191817161312111096543229Nov282726252221201815126added bib filedocumentation/d…documentation/documentation_aerodynamic_analysisIntroduction of propFus Strategy and implementation of first method partI hate mergesMerge remote-tracking branch 'origin/documentation/documentation_aerodynamic_analysis' into documentation/documentation_aerodynamic_analysisRevisions to the docApply 1 suggestion(s) to 1 file(s)Apply 1 suggestion(s) to 1 file(s)Apply 1 suggestion(s) to 1 file(s)Copied some values in new dict entry for output compatibilityMade some corrections (especially to CoG).commit pipfileBA_NLFBA_NLFAnd new progressMerge branch 'feature/cost_estimation_add_html_report' into 'develop'Feature/cost estimation add html reportAdded some functionalities.Initial versionInitial commit. Tandem template creation for development.novel progresswith naccele cm correction mode_2, L/D is higherfix/search_for_…fix/search_for_CM_problemMade some further changesMerge branch 'feature/tank_design_add_html_report' into 'develop'tank_design: Method HTML report implementationMerge branch 'fix/systems_engine_placement' into 'develop'Add empennage as possible engine postion in systems_designMerge branch 'feature/flight_mechanic_assessment_cs25_149' into 'feature/flight_mechanic_assessment'calculateconicaltank.py: Added available volume to output dict.Initial SetupMerge branch 'fix/update_inkscape_and_gnuplot_path' into 'develop'Adapted files to changes._02_preparegeometricaldata.py:_01_checktankconfiguration.py:_01_checktankconfiguration.py:Addressed review commentsAdresses issue #33 -> replace default by ../gnuplot/ and ../inkscape/Add delta ISAfix/initial_siz…fix/initial_sizing_delta_ISAMerge branch 'feature/have_more_output_in_propulsion_design_mode_1' into 'develop'Reworked export functions: html, plot and xmlAdded output dict as an output for the assess-functionAdded CS25.149 as a new criteriaUpdated path to cs25_assessment.xml to work from flight mechanic assessment
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