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  • 63-wrong-vertical-wing-position-when-mounting-set-to-high
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Created with Raphaël 2.2.014Apr111097432131Mar2928272625242221201918171615141312111086528Feb27262524222120191817161413121097654331Jan3029282725242322212017161514131098763220Dec19181716fuselage_design: - hotFix: update tube and wing mass estimation to fix dictionary errorMerge branch 'feature/fuselage_design_updates' into 'main'fuselage_design: - update of blended wing body code regarding the modularization conceptImproved error handling in create_mission_xmlCHange further ; position and delete unnecessary indexApply 6 suggestion(s) to 3 file(s)Change airports.csvChanges to be sure that correct range is used by all modulesMerge branch 'fix/wb_remove_warning_plot' into 'main'Removed plot warningMerge branch 'fix/aero_for_B_double_U_B' into 'main'deleted unnecessary console outputsApply 1 suggestion(s) to 1 file(s)Apply 1 suggestion(s) to 1 file(s)Apply 1 suggestion(s) to 1 file(s)Merge branch 'feature/BA_fauzan' of git.rwth-aachen.de:unicado/aircraft-design into feature/BA_fauzanfeature/BA_fauzanfeature/BA_fauzannow is workingmodifief path for aero and dataprepoctestCorrections and improved error handlingtook mass prop out from treelocal paths updatedShift airports.csv into libs folderAdd airports switch and improved plot in mission_analysisnew EMPBA with main but still have problem in postprocessingadd missing changes in last commitAdd plot in mission_analysisChanges on create_mission_xmlfinished visc drag fixim not able to generate html reports for the BWBfirst draft in mission_analysisadaptions for create_mission- write to acxml: separate design and study mission blocks and added descriptionshigh lift polar spits out numbers nowcleanupsrange calculation according to given origin and destination airportfeature/develop…feature/develop_airtimeMerge branch 'fix/remove_oxygen_system_from_systems_design' into 'main'Fix/remove oxygen system from systems design- different reports for the design and study missiondoing important scientific and engineering stuffeleminated fuselage geometry from wave drag calculation
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