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UNICADO
Aircraft Design
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f5cc0f247dbfa53842a9cb64a63a6576235fa849
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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/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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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
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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'
Feature/cost estimation add html report
Added some functionalities.
Initial version
Initial commit. Tandem template creation for development.
novel progress
with naccele cm correction mode_2, L/D is higher
fix/search_for_…
fix/search_for_CM_problem
Made some further changes
Merge branch 'feature/tank_design_add_html_report' into 'develop'
tank_design: Method HTML report implementation
Merge branch 'fix/systems_engine_placement' into 'develop'
Add empennage as possible engine postion in systems_design
Merge branch 'feature/flight_mechanic_assessment_cs25_149' into 'feature/flight_mechanic_assessment'
calculateconicaltank.py: Added available volume to output dict.
Initial Setup
Merge branch 'fix/update_inkscape_and_gnuplot_path' into 'develop'
Adapted files to changes.
_02_preparegeometricaldata.py:
_01_checktankconfiguration.py:
_01_checktankconfiguration.py:
Addressed review comments
Adresses issue #33 -> replace default by ../gnuplot/ and ../inkscape/
Add delta ISA
fix/initial_siz…
fix/initial_sizing_delta_ISA
Merge branch 'feature/have_more_output_in_propulsion_design_mode_1' into 'develop'
Reworked export functions: html, plot and xml
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