Issue Analytics

Overview

Opened

Avg: 4.46 · Max: 27

Closed

Avg: 9.46 · Max: 36

Issue	Age	Status	Milestone	Due date	Assignees	Created by
Broken Endnode @multi_passenger_deck_layout #192 2	2 days	Opened	Beta v0.6.0			G
Aircraft Geometry and CGAL Coordinates #191 3	11 days	Closed	Milestone Final v1.0		3 additional assignees	L
Set TOM and CG for study mission #190 2	12 days	Opened	Beta v0.6.0			G
bwb_geometry: wing_design_conf element error #189 3	15 days	Closed	Beta v0.6.0			F
fuselage_design: resolve problems in blended_wing_body strategy #188 3	15 days	Opened	Beta v0.6.0			F
initial_sizing: Add analytical strategy for blended_wing_body #187 3	15 days	Opened	Beta v0.6.0			F
Faulty Ceiling Calculation #186 &18 2	15 days	Opened	Beta v0.6.0			P
Update wing_design module to handle tube_and_wing and blended_wing_body configuration #185 2	17 days	Opened	Beta v0.6.0			F
Bug inertia calculation #184 &18 2	22 days	Closed	Beta v0.6.0			T
Implement new method using calibration based on higher fidelity data #183 2	22 days	Opened	Milestone Final v1.0			K
Implement adaption to existing geometry mode #182 &24 1	22 days	Opened	Beta v0.7.0			K
Check reference year correction #181 2	22 days	Opened	Milestone Final v1.0			K
Make outputs in dollar #180 2	22 days	Opened	Milestone Final v1.0			K
Discuss if the V-n diagram can be included in the constraint_analysis #179 2	22 days	Opened	Milestone Final v1.0			K
Check if LTO is already checked and can be skipped #178 2	22 days	Opened	Milestone Final v1.0			K
Landing errors (thrust reverser and landing field length) #177 &18 2	22 days	Closed	Beta v0.6.0			G
Implement higher fidelity method for PR diagram #176 &23 2	22 days	Opened	Beta v0.7.0			K
Discuss if initial_sizing and constraint_analysis can be merged into one tool #175 2	22 days	Opened	Milestone Final v1.0			K
Discuss if limit equations should be provided as libraries #174 2	22 days	Opened	Milestone Final v1.0			K
Include top-of-climb and approach speed limit #173 2	22 days	Opened	Milestone Final v1.0			K
Discuss what CLmax is written in the acXML by aerodynamic_analysis #172 2	22 days	Opened	Milestone Final v1.0			K
Update config xml #171 2	22 days	Opened	Milestone Final v1.0			K
Calculate CG shift in air #170 &35 2	22 days	Opened	Beta v0.9.0			K
Calculate dive speed for landing_gear_design #169 2	22 days	Opened	Milestone Final v1.0			K
Get vector of aircraft masses from weight_and_balance_analysis #168 &35 2	22 days	Opened	Beta v0.9.0			K
Simplify standard mission method by eliminating mission below FL15 #167 2	22 days	Opened	Milestone Final v1.0			K
Reduce multiple precision settings to one (time increment) #166 2	22 days	Opened	Milestone Final v1.0			K
aerodynamic_analysis: reactivate adapt polars to cruise Mach number #161 3	38 days	Opened	Milestone Final v1.0		2 additional assignees	F
systems_design: implement a low fidelity method #160 2	38 days	Opened	Milestone Final v1.0			K
Aerodynamic_analysis: check high-lift angle of attack #159 2	38 days	Opened	Milestone Final v1.0		1 additional assignee	K
propulsion_design & landing_gear_design: Discuss how to handle interference if pushed to much outboards #158 2	38 days	Opened	Milestone Final v1.0		1 additional assignee	K
landing_gear_design: implement a low fidelity method #157 2	38 days	Opened	Milestone Final v1.0			K
landing_gear_design: Adapt maximum achievable CL #156 1	38 days	Opened	Milestone Final v1.0			K
propulsion_design: empirical method execution #155 &23 2	38 days	Opened	Beta v0.7.0			K
propulsion_design & aerodynamic_analysis: shift nacelle drag to net thrust #154 2	38 days	Opened	Milestone Final v1.0			K
empennage_design: include new method resizing acc to stability #153 2	38 days	Opened	Milestone Final v1.0			K
fuselage_design: implement a low fidelity method #152 2	39 days	Opened	Milestone Final v1.0			K
initial_sizing: calculate fuel mass with MTOM-OME-PL #151 1	39 days	Opened	Milestone Final v1.0			K
Initial_sizing: include method in which user can set performance parameter in the config #150 &24 2	39 days	Closed	Beta v0.7.0			K
Extract a point_performance_analysis tool from mission_analysis #149 2	39 days	Opened	Milestone Final v1.0		1 additional assignee	K
set intial thrust: Unresonable acceleration in cruise segment #148 2	43 days	Closed				L
Manual specification of steps climbs / descends #147 2	43 days	Opened				L
Export CoG-Shift for Mission Analysis #145 2	46 days	Closed	Milestone Final v1.0			G
Operating item scaling factor not working #144 2	51 days	Closed				L
Mass scaling factor for furnishings #143 2	51 days	Closed				L
Mass scaling factor separate for VTP and HTP #142 &18 2	51 days	Opened	Beta v0.6.0			L
Wrongly displayed alternate distance #140 &18 2	51 days	Closed	Beta v0.6.0			G
Python framework: Expected data type check update #136 1	68 days	Opened				S
weight_and_balance_analysis: enable run without seat_positions.xlsx #105 &16 3	73 days	Closed	Milestone Breguet			K
Bleed air in unit W instead of kg/s #70	107 days	Closed				T
Required Take-Off Parameter for landing gear design #69 2	109 days	Closed				A
Aerodynamic analysis: enable higher AoA in cruise #66 3	113 days	Opened			3 additional assignees	K
propulsion_design: - energie efficiency technology factor doesn't work in current version of propulsion_design module #65 2	113 days	Closed	Milestone Dornier			A
Landing gear design: enable fuselage mounting #64 3	113 days	Opened				K
Wrong vertical wing position when mounting set to "high" #63 2	114 days	Closed				J
Wrong program abort for unknown config values #54 2	120 days	Closed	Milestone Dornier	2024-12-12		F
Delete bwb config in all tools #53 1	120 days	Closed	Milestone Torenbeek			K
CI pipeline for aircraft design repository shall be extended to test on windows #101 &26 2	190 days	Opened	Beta v0.8.0			M