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  • 63-wrong-vertical-wing-position-when-mounting-set-to-high
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Created with Raphaël 2.2.021Apr17161514111097432131Mar2928272625242221201918171615141312111086528Feb27262524222120191817161413121097654331Jan3029282725242322212017161514131098763220Dec19comment correctionsfeature/tandem_…feature/tandem_BA_Yazici- added the tank mass to the structure groupfix/wb_h2_tanksfix/wb_h2_tanks- took the used_tank flags outfix/wb_fuel_unu…fix/wb_fuel_unused_tanksbug fix unused tanks -> if a tank is available but not used during mission, it is assumed 0 kg of fuel in this tank.Fix of false calculation of the design payload. The max payload was read from the acXML instead of calculating the design payloadfix/performance…fix/performance_assessment-payload-range_calculationMerge branch 'fix/performance_assessment_ceiling_calculation' into 'main'fix/aerodynamic…fix/aerodynamic_analysis_html_report_fix main- added switch to change between design and study mission based on the mission_config_file.xmlfeature/wb_stud…feature/wb_study_modeApply 3 suggestion(s) to 2 file(s)- methodhtmlreport.py: Deleted total energy information data.fix/tank_design…fix/tank_design_fix_maximum_energy_capacity_and_remove_flags- datapostprocessing.py: Deleted path to `energy_capacity_required_for_mission` from key parameter paths list, deleted parameter from key parameter dictMerge branch 'fix/aerodynamic_analysis_terminate_plotting' into 'main'feature/NLFfeature/NLFRenamed outputs for writing to acxml under the design and study missionFix aerodynamic_analysis gnuplot not terminating issueMerge branch 'feature/fuselage_design_updates' into 'main'Feature/fuselage design updatesbetter description for visc drag calibrationfix/better_desc…fix/better_descriptionsMerge branch 'hotfix/CODEOWNERS' into 'main'aircraft_design (schueltke):Refactored mass technology-factor: removed global, added per-stabilizerfeature/seperat…feature/seperate_scaling_factors_empennagele sweep in buffet calculation is now calculated at macfix/buffet_onsetfix/buffet_onsetMerge branch 'feature/fuselage_design_updates' into 'main'fuselage_design_ - hotFix: rename lightning to lightingAdd brackets againfix/allow_highe…fix/allow_higher_machMerge branch 'main' into bug/allow_higher_machInterrupt SAR plot loop if max_ma is exceededDelete "not implemented" in configfeature/4d-traj…feature/4d-trajectoryMerge 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 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)
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