Ecosyste.ms: Issues
An open API service for providing issue and pull request metadata for open source projects.
GitHub / supaero-aircraft-design/FAST-GA issues and pull requests
#222 - Advanced MFW computation revamped
Pull Request -
State: open - Opened by florentLutz about 1 month ago
#221 - Developper environment update + Ruff usage + Minor fixes
Pull Request -
State: closed - Opened by florentLutz 2 months ago
- 1 comment
#220 - Implement Minimum Induced Loss method for propeller
Issue -
State: open - Opened by florentLutz 6 months ago
#219 - Release 1.3.0
Pull Request -
State: closed - Opened by florentLutz 6 months ago
#218 - Compatibility with Python 3.10
Pull Request -
State: closed - Opened by florentLutz 6 months ago
#217 - Optimization of turboprop model
Pull Request -
State: closed - Opened by florentLutz 6 months ago
- 1 comment
#216 - Complete polar database
Pull Request -
State: closed - Opened by florentLutz 7 months ago
- 1 comment
#215 - Improvement of aerodynamic tools
Pull Request -
State: closed - Opened by florentLutz 8 months ago
- 1 comment
#214 - Release v1.2.2
Pull Request -
State: closed - Opened by florentLutz 8 months ago
#213 - Update Release process
Pull Request -
State: closed - Opened by florentLutz 8 months ago
#212 - Release v1.2.1
Pull Request -
State: closed - Opened by florentLutz 8 months ago
#211 - Bug correction for new package version
Pull Request -
State: closed - Opened by florentLutz 8 months ago
- 1 comment
Labels: bug
#210 - Incohérence flap_types
Issue -
State: open - Opened by lusanchez1 8 months ago
#209 - Analytical Derivative Implementation
Pull Request -
State: closed - Opened by Muhabdaziz about 1 year ago
#208 - Model sequencing optimizer
Pull Request -
State: closed - Opened by bielgaliot about 1 year ago
#207 - Improve aerodynamic tools and readability
Pull Request -
State: closed - Opened by johnathanasd about 1 year ago
#206 - Allowing newer version of stdatm
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
- 1 comment
#205 - Change in the version of poetry
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
#204 - "data:propulsion:fuel_type"=3 erreur avec modèle géométrique simple
Issue -
State: open - Opened by mariesouffez over 1 year ago
#203 - Release v1.2.0
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
#202 - Development of high wing models
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
- 3 comments
#201 - Merging of intership work on wing geometry
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
#200 - Upstream/fomra
Pull Request -
State: closed - Opened by fomra over 1 year ago
#199 - VLM code / TBM example
Issue -
State: closed - Opened by mariesouffez over 1 year ago
#198 - Upstream/fomra
Pull Request -
State: closed - Opened by fomra over 1 year ago
#197 - Support issues for Numpy 1.24.0
Issue -
State: closed - Opened by florentLutz over 1 year ago
- 1 comment
#196 - Added yml as a viable input for the block analysis
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
- 1 comment
#195 - Dev partial derivatives
Pull Request -
State: closed - Opened by florentLutz over 1 year ago
#194 - Improvement: Block Analysis from .yml
Issue -
State: closed - Opened by florentLutz almost 2 years ago
#193 - Dev issue 188
Pull Request -
State: closed - Opened by florentLutz almost 2 years ago
- 1 comment
#192 - Release v1.1.0
Pull Request -
State: closed - Opened by florentLutz almost 2 years ago
- 1 comment
#191 - Fill in drag coefficient in mission FlightPoints
Issue -
State: closed - Opened by esnguyenvan almost 2 years ago
#190 - Fixing mass update formula
Pull Request -
State: closed - Opened by florentLutz almost 2 years ago
- 1 comment
#189 - Review mass update in mission vector
Issue -
State: closed - Opened by florentLutz almost 2 years ago
#188 - Generalize use of @functools.lru_cache
Issue -
State: closed - Opened by florentLutz almost 2 years ago
Labels: enhancement
#187 - Save flight points
Pull Request -
State: closed - Opened by esnguyenvan almost 2 years ago
- 8 comments
#186 - Remove math import
Issue -
State: closed - Opened by florentLutz almost 2 years ago
#185 - Addition of the computation of aerodynamic derivatives
Pull Request -
State: closed - Opened by florentLutz almost 2 years ago
- 3 comments
#184 - Improve single AoA launch
Issue -
State: closed - Opened by florentLutz about 2 years ago
#183 - Xfoil in inviscid mode
Issue -
State: closed - Opened by florentLutz about 2 years ago
#182 - Fix xfoil
Pull Request -
State: closed - Opened by florentLutz about 2 years ago
#181 - Add unit for CnBeta fuselage
Issue -
State: closed - Opened by florentLutz about 2 years ago
#180 - Add formula for double slotted flap
Issue -
State: open - Opened by florentLutz about 2 years ago
#179 - Imrpove Xfoil interface
Issue -
State: closed - Opened by florentLutz about 2 years ago
#178 - Release v1.0.4
Pull Request -
State: closed - Opened by florentLutz about 2 years ago
#177 - Dev vlm improvement
Pull Request -
State: closed - Opened by florentLutz about 2 years ago
- 1 comment
#176 - Dev bemt improvement
Pull Request -
State: closed - Opened by florentLutz about 2 years ago
#175 - The k-factors for the HTP from VLM and OpenVSP are different
Issue -
State: open - Opened by NOTaShinigami about 2 years ago
#174 - Improve compressibility and viscosity corrections in BEMT code
Issue -
State: closed - Opened by florentLutz about 2 years ago
#173 - An incorrect variable is being used to compute the aircraft's cl_alpha (VLM method)
Issue -
State: closed - Opened by NOTaShinigami about 2 years ago
- 1 comment
#172 - Dev prop improvement
Pull Request -
State: closed - Opened by florentLutz about 2 years ago
#171 - Generic mass breakdown
Issue -
State: open - Opened by florentLutz about 2 years ago
- 1 comment
Labels: bug
#170 - Propeller performances as classic maps
Issue -
State: closed - Opened by florentLutz about 2 years ago
#169 - Add the possibility to specify the path to airfoil resources
Issue -
State: closed - Opened by florentLutz about 2 years ago
#168 - Update CHANGELOG.rst
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#167 - Import post_processing function in API
Issue -
State: open - Opened by florentLutz over 2 years ago
- 1 comment
#166 - Remove use of matplotlib in analysis_and_plots
Issue -
State: closed - Opened by florentLutz over 2 years ago
Labels: bug
#165 - Update CHANGELOG.rst
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#164 - Release v1.0.1
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#163 - Release v1.0.0
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#162 - Dev proper fastoad import
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#161 - Dev tbm 900
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#160 - Add the computation of the stability derivative using OpenVSP
Issue -
State: open - Opened by florentLutz over 2 years ago
#159 - Dev codacy issue correction
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#158 - Generalize use of fastoad.api instead of direct import
Issue -
State: closed - Opened by florentLutz over 2 years ago
#157 - Dev new mission
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#156 - Dev propulsion adjustments
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#155 - Add a method to compute Vh which is based on the new equilibrium block.
Issue -
State: open - Opened by florentLutz over 2 years ago
#154 - Dev mission improvement
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#153 - Dev reference aircraft
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#152 - Formulae in the TASOPT ocumentation could be used to compute lift distribution without VLM
Issue -
State: open - Opened by florentLutz over 2 years ago
#151 - Study the viability of the transposition of the wing mass estimation methodology for other lifting surface.
Issue -
State: open - Opened by florentLutz over 2 years ago
- 2 comments
#150 - Modify usage of dataframe inside the mission
Issue -
State: closed - Opened by florentLutz over 2 years ago
#149 - Study the compatibility with OpenMDAO 3.17.0 (recommended for recorder ussage)
Issue -
State: closed - Opened by florentLutz over 2 years ago
#148 - Dev turboprop
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 2 comments
#147 - Dev partial derivatives
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#146 - Add possibility to change CRUD factor in cd0 total computation
Issue -
State: closed - Opened by florentLutz over 2 years ago
#145 - Add propeller performance post-processing tool
Issue -
State: closed - Opened by florentLutz over 2 years ago
#144 - Dev issue 143
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#143 - Suboptimal polar result reading in propeller performance computation
Issue -
State: closed - Opened by florentLutz over 2 years ago
#142 - Dev issue correction
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#141 - Add coverage on post-processing
Issue -
State: closed - Opened by florentLutz over 2 years ago
Labels: enhancement
#140 - Dev fast oad 1 3 1
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
#139 - Dev mass model
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#138 - Dev fast oad 1 3 0
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
#137 - Added the computation of 2D aerodynamic effects of flaps
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 1 comment
Labels: enhancement, aerodynamics
#136 - Issue 131 propeller leading edge
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
Labels: enhancement, geometry
#135 - Separation of wing area model
Pull Request -
State: closed - Opened by florentLutz over 2 years ago
- 2 comments
Labels: enhancement, aerodynamics, geometry
#133 - Wing mass loop sizing case should be separated
Issue -
State: closed - Opened by florentLutz over 2 years ago
Labels: enhancement, aerodynamics, geometry
#132 - Tutorial 2 : Equilibrated Polar computation shows unfeasible points
Issue -
State: closed - Opened by florentLutz over 2 years ago
#131 - Distance between propeller and leading edge
Issue -
State: closed - Opened by florentLutz over 2 years ago
#127 - Dev codacy issue v2
Pull Request -
State: closed - Opened by florentLutz almost 3 years ago
#123 - Change the computation of the landing gear CoG with an implicit component compared to the global CoG of the Aircraft
Issue -
State: closed - Opened by florentLutz almost 3 years ago
#117 - Change the taxi speed
Issue -
State: closed - Opened by florentLutz almost 3 years ago
#115 - Updated poetry.lock and bug correction
Pull Request -
State: closed - Opened by florentLutz almost 3 years ago
#114 - Dev polars
Pull Request -
State: closed - Opened by florentLutz almost 3 years ago
#113 - Lucas test
Pull Request -
State: closed - Opened by florentLutz almost 3 years ago
#111 - Change the "quantity" of turbulent flow on the wing depending on the placement of the engine (if behind engine == turbulent) ?
Issue -
State: closed - Opened by florentLutz almost 3 years ago
#110 - Put a failsafe on cruise computation if the distance is 0.
Issue -
State: closed - Opened by florentLutz about 3 years ago
#109 - The value of the mean rpm used for propeller computation should be an option or an input
Issue -
State: closed - Opened by florentLutz about 3 years ago