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  • 63-wrong-vertical-wing-position-when-mounting-set-to-high
  • BA_NLF
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Created with Raphaël 2.2.014Apr11109432131Mar29282726252422212019181716141312111086528Feb27262524222120191817161413121097654331Jan3029282725242322212017161514131098763220Dec19181716fuselage_design_ - hotFix: rename lightning to lightingMerge branch 'feature/fuselage_design_updates' into 'main'fuselage_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 conceptMerge 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 dataprepoctesttook mass prop out from treelocal paths updatednew EMPBA with main but still have problem in postprocessingfinished visc drag fixim not able to generate html reports for the BWB- 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 airportMerge 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 calculationwave drag mason to goit is compilable againylim payload range diagram changedfirst stepsMerge branch 'feature/neuer_zweig' into 'main'Feature/neuer zweigMerge branch 'fix/landing_gear_design' into 'main'landing_gear_design: - fix minimum percentage of nose gear load error for...Hardcoded required ROC to 100ft/min (50ft/min OEI) for "fan" propulsion and 50ft/min for "prop" propulsionFurther development of the ORF integration now on tandem wing and at the top of the fuselagefeature/propuls…feature/propulsion_design_open_rotorAdd center of gravity of individual systems to acxml and adapt path in ecological assessmentfeature/individ…feature/individual_system_CoGs_in_acxml