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UNICADO
Aircraft Design
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d3c1f69b3d4d21934d62d3cdac96f942cee1f03e
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Branches
20
63-wrong-vertical-wing-position-when-mounting-set-to-high
BA_NLF
BA_Stangier
BA_Szklarczyk
BA_Yazici
beta_release
protected
documentation/aircraft_design
documentation/documentation_aerodynamic_analysis
feature/185-update-wing_design-module-to-handle-tube_and_wing-and-blended_wing_body-configuration
feature/4d-trajectory
feature/BA_fauzan
feature/CI_build
feature/NLF
feature/aero_html_loick
feature/aero_new_plots
feature/aero_report_improvement
feature/aeroelastic_analysis
feature/auto_flight_conditions
feature/constraint_analysis_updates
feature/constraint_analysis_workaround
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6
0.5.0
0.4.0
0.3.1
0.3.0
0.2.0
0.1.0
26 results
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Created with Raphaël 2.2.0
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comment corrections
feature/tandem_…
feature/tandem_BA_Yazici
- added the tank mass to the structure group
fix/wb_h2_tanks
fix/wb_h2_tanks
- took the used_tank flags out
fix/wb_fuel_unu…
fix/wb_fuel_unused_tanks
bug 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 payload
fix/performance…
fix/performance_assessment-payload-range_calculation
Merge 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.xml
feature/wb_stud…
feature/wb_study_mode
Apply 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 dict
Merge branch 'fix/aerodynamic_analysis_terminate_plotting' into 'main'
feature/NLF
feature/NLF
Renamed outputs for writing to acxml under the design and study mission
Fix aerodynamic_analysis gnuplot not terminating issue
Merge branch 'feature/fuselage_design_updates' into 'main'
Feature/fuselage design updates
better description for visc drag calibration
fix/better_desc…
fix/better_descriptions
Merge branch 'hotfix/CODEOWNERS' into 'main'
aircraft_design (schueltke):
Refactored mass technology-factor: removed global, added per-stabilizer
feature/seperat…
feature/seperate_scaling_factors_empennage
le sweep in buffet calculation is now calculated at mac
fix/buffet_onset
fix/buffet_onset
Merge branch 'feature/fuselage_design_updates' into 'main'
fuselage_design_ - hotFix: rename lightning to lighting
Add brackets again
fix/allow_highe…
fix/allow_higher_mach
Merge branch 'main' into bug/allow_higher_mach
Interrupt SAR plot loop if max_ma is exceeded
Delete "not implemented" in config
feature/4d-traj…
feature/4d-trajectory
Merge branch 'feature/fuselage_design_updates' into 'main'
fuselage_design: - hotFix: update tube and wing mass estimation to fix dictionary error
Merge branch 'feature/fuselage_design_updates' into 'main'
fuselage_design: - update of blended wing body code regarding the modularization concept
Improved error handling in create_mission_xml
CHange further ; position and delete unnecessary index
Apply 6 suggestion(s) to 3 file(s)
Change airports.csv
Changes to be sure that correct range is used by all modules
Merge branch 'fix/wb_remove_warning_plot' into 'main'
Removed plot warning
Merge branch 'fix/aero_for_B_double_U_B' into 'main'
deleted unnecessary console outputs
Apply 1 suggestion(s) to 1 file(s)
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