Skip to content
GitLab
Explore
Sign in
Primary navigation
Search or go to…
Project
Aircraft Design
Manage
Activity
Members
Labels
Plan
Issues
Issue boards
Milestones
Iterations
Wiki
Requirements
Code
Merge requests
Repository
Branches
Commits
Tags
Repository graph
Compare revisions
Snippets
Locked files
Build
Pipelines
Jobs
Pipeline schedules
Test cases
Artifacts
Deploy
Releases
Package registry
Container registry
Model registry
Operate
Environments
Terraform modules
Monitor
Incidents
Service Desk
Analyze
Value stream analytics
Contributor analytics
CI/CD analytics
Repository analytics
Code review analytics
Issue analytics
Insights
Model experiments
Help
Help
Support
GitLab documentation
Compare GitLab plans
Community forum
Contribute to GitLab
Provide feedback
Terms and privacy
Keyboard shortcuts
?
Snippets
Groups
Projects
Show more breadcrumbs
UNICADO
Aircraft Design
Repository graph
Repository graph
You can move around the graph by using the arrow keys.
ea3e3bca094d2a601deff1afa88437e3974a126b
Select Git revision
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/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
Tags
6
0.5.0
0.4.0
0.3.1
0.3.0
0.2.0
0.1.0
26 results
Begin with the selected commit
Created with Raphaël 2.2.0
15
Jan
14
13
10
9
8
7
6
3
2
20
Dec
19
18
17
16
13
12
11
10
9
6
5
4
3
2
29
Nov
28
27
26
25
22
21
20
18
15
12
6
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'
Added constraint analysis
calculatetanks.py: Corrected location of 'total_tank_parameters' subdictionary definition
Made a few adaptions
Merge branch 'develop' of ssh://git.rwth-aachen.de/unicado/aircraft-design into develop
Integrate pyenergy_carriers
feature/wb_ener…
feature/wb_energy_carriers_lib
enabled design of turbofan engine with liquid hydrogen as energy carrier
feature/propuls…
feature/propulsion_hydrogen
Merge branch 'fix/atm_ISA_setting' into 'develop'
Fix for MissionAnalysis: take delta ISA into account
added bib file
documentation/d…
documentation/documentation_aerodynamic_analysis
Introduction of propFus Strategy and implementation of first method part
I hate merges
Merge remote-tracking branch 'origin/documentation/documentation_aerodynamic_analysis' into documentation/documentation_aerodynamic_analysis
Revisions to the doc
Apply 1 suggestion(s) to 1 file(s)
Apply 1 suggestion(s) to 1 file(s)
Apply 1 suggestion(s) to 1 file(s)
Copied some values in new dict entry for output compatibility
Made some corrections (especially to CoG).
commit pipfile
BA_NLF
BA_NLF
And new progress
Merge branch 'feature/cost_estimation_add_html_report' into 'develop'
Loading