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UNICADO
Aircraft Design
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9ace8f1d85e32e25c169dd832a897f09a48cf01f
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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/BA_fauzan
feature/CI_build
feature/CI_build_bb
feature/CI_build_perf
feature/NLF
feature/aero_html_loick
feature/aero_new_plots
feature/aero_report_improvement
feature/aerodynamic_analysis_sbw
feature/aerodynamic_analysis_tandem
feature/aeroelastic_analysis
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26 results
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Created with Raphaël 2.2.0
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Feature/fuslage design
Aanother small cleanup
Small cleanup
Fixed issues
Merge branch 'fix/systems_design_delta_ISA' into 'develop'
Fix use of delta_ISA in systems_design
intermediate save
Merge branch 'fix/aerodynamic_analysis' into 'develop'
Make aero analysis buildable
Did some cleaning and tried to make stuff more readable
Made some changes for html output
feature/tank_de…
feature/tank_design_liquid_hydrogen
Increase readability
Merge branch 'feature/aero_html_report' into 'develop'
Add aerodynamic_analysis html report
Merge branch 'feature/landing_gear_design_html_report' into 'develop'
landing_gear_design: Add HTML report function
Merge branch 'feature/fuselage_design_add_html_output' into 'develop'
fuselage_design: Add HTML report function
Merge branch 'feature_one_more_command_output' into 'develop'
deletes stupid comment
Adds one line to the console which is always printing to have the main stuff in there (T/W, MTOM and overall THurst)
Merge branch 'fix/aero_delta_isa_zeugs' into 'develop'
Apply 1 suggestion(s) to 1 file(s)
Apply 1 suggestion(s) to 1 file(s)
Apply 1 suggestion(s) to 1 file(s)
Apply 1 suggestion(s) to 1 file(s)
Apply 1 suggestion(s) to 1 file(s)
trim testing using casadi -> working (fast)
made files casadi feasible
active CS25.181
Merge branch 'feature/propulsion_hydrogen' into 'develop'
added delta T for ISA in all methods and strategies
use gravimetric energy density and emission indices of energyCarrier lib
changed a few things
Merge branch 'develop' of ssh://git.rwth-aachen.de/unicado/aircraft-design into develop
datapostprocessing.py: Added paths and dict entries for LH2 output
Merge branch 'feature/decrease_mission_segment_inputs' into 'develop'
Feature/decrease mission segment inputs
Merge branch 'feature/tank_design_correct_total_tank_parameter' into 'develop'
Merge branch 'feature/constraint_analysis' into 'develop'
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