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  • 63-wrong-vertical-wing-position-when-mounting-set-to-high
  • BA_NLF
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Created with Raphaël 2.2.09May8765230Apr2928252423222116151411109432131Mar29282726252422212019181716141312111086528Feb27262524222120191817161413121097654331Jan302928272524232221201716151413109Back to python3feature/CI_buil…feature/CI_build_perfNow performance test with python aliasKleine Änderungfeature/NLFfeature/NLFEs funktioniertDo not delete .git folderUpdated unicado headless installerFix typoCopied performance test from other repo + first adaptionsMinor correctionfeature/CI_buil…feature/CI_build_bbAlternative airfoil data folderCopy database directly into aircraft project folderMerge branch 'feature/create_mission_with_step_descent' into feature/develop_airtimefeature/develop…feature/develop_airtimeAdd database folders, since they are needed by some modulesFixed wrong default mode in configfeature/create_…feature/create_mission_with_step_descentMinor changes (e.g. reintroduced ICA autoselect)Add missing libraries to run the black-box tests. Probably for the python tools python3 and python3-dev must be installed anywayChanged diff range, since a newly created branch has no predecessorfeature/CI_buildfeature/CI_buildCorrected diff range also for integration_test. Switched name from engineSizing to propulsion_designMerge branch 'feature/step_climb_descent' into feature/develop_airtimeTry diff against merge base from HEAD and origin/mainFirst test of black-box test with new repo structureCMake angepasstMerge branch 'main' into feature/develop_airtimeadaption in mode FLCHANGE to allow step descendsfeature/step_cl…feature/step_climb_descentDelete even more obsolete filesDeleted obsolete filesVielleicht klappts jetztStand 16:22Integration of Tandem wing in aerodynamic_analysis as until now in BA Yazici, not completedfeature/aerodyn…feature/aerodynamic_analysis_tandemProbiert das Regressionsmodell hinzuzufügenMerge branch 'feature/fuselage_design_updates' into 'main'mainmainDo not delete design_evaluator folder, to keep the resultsNew aircraft names and pathsChanged branches to mainfuselage_design: - bug fix: x-coordinates of LH2 fuselages are now correctUpdates from mainMerge branch 'feature/fuselage_design_updates' of ssh://git.rwth-aachen.de/unicado/aircraft-design into feature/fuselage_design_updatesFix some indices for wing_design plotfix/wing_design…fix/wing_design_indices_visualizationAdded liftingLineForSBW to account for one entry more in fuselageWidths, thus correcting error in liftingLineinterface. Tested and runs. Report generation not succesfulfeature/aerodyn…feature/aerodynamic_analysis_sbwSBW Implementation as done by BA Wischmeyer in Aerodynamic_analysis