Skip to content

Issues: supaero-aircraft-design/FAST-GA

Support issues for Numpy 1.24.0
#197 by florentLutz was closed Feb 16, 2024
Closed 1
New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

Sign up for GitHub

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

38 Open 103 Closed
38 Open 103 Closed
Author
Filter by author
Label
Filter by label
Use alt + click/return to exclude labels
or ⇧ + click/return for logical OR
Projects
Filter by project
Milestones
Filter by milestone
Assignee
Filter by who’s assigned
Sort
Sort by
Newest Oldest Most commented Least commented Recently updated Least recently updated Best match
Most reactions
👍 👎 😄 🎉 😕 ❤️ 🚀 👀

Issues list

Implement Minimum Induced Loss method for propeller
#220 opened Apr 3, 2024 by florentLutz
Incohérence flap_types
#210 opened Feb 7, 2024 by lusanchez1
"data:propulsion:fuel_type"=3 erreur avec modèle géométrique simple
#204 opened Mar 21, 2023 by mariesouffez
@florentLutz
Add formula for double slotted flap
#180 opened Sep 27, 2022 by florentLutz
The k-factors for the HTP from VLM and OpenVSP are different
#175 opened Aug 26, 2022 by NOTaShinigami
Generic mass breakdown bug Something isn't working
#171 opened Aug 4, 2022 by florentLutz
@florentLutz
1
Import post_processing function in API
#167 opened Jun 2, 2022 by florentLutz
1
Add the computation of the stability derivative using OpenVSP
#160 opened May 30, 2022 by florentLutz
Add a method to compute Vh which is based on the new equilibrium block.
#155 opened May 13, 2022 by florentLutz
Formulae in the TASOPT ocumentation could be used to compute lift distribution without VLM
#152 opened May 6, 2022 by florentLutz
Study the viability of the transposition of the wing mass estimation methodology for other lifting surface.
#151 opened May 6, 2022 by florentLutz
2
Cruise altitude for propeller
#116 opened Nov 3, 2021 by florentLutz
Vérifier si une mise-à-jour des formules de masse est nécessaire enhancement New feature or request good first issue Good for newcomers weight & cg For issue that relates to computations in the weight module
#101 opened Aug 25, 2021 by florentLutz
1
Ajouter le fuel non utilisé dans le mass breakdown methodology For issue that requires a change in the formula and/or the computation methodology weight & cg For issue that relates to computations in the weight module
#100 opened Aug 24, 2021 by florentLutz
Faire une fonction de calcul du plafond de poussée
#99 opened Aug 3, 2021 by florentLutz
Ecrire proprement la bibliographie comme expliqué dans le wiki FAST OAD
#98 opened Aug 2, 2021 by florentLutz
Revoir la définition géométrique de la partie cylindrique du fuselage notamment les calculs de maximum_height et maximum_width
#93 opened Jul 28, 2021 by florentLutz
Changer le calcul des performances hélices pour prendre en compte le cas où le pitch est fixé et la poussée est reglée par les RPM
#89 opened Jul 26, 2021 by florentLutz
Rajouter un vecteur de masses ponctuelles dans le XML
#85 opened Jul 20, 2021 by florentLutz
Comparer résultat des calculs de Cd0 à OpenVSP
#82 opened Jul 20, 2021 by florentLutz
Séparer la propulsion en deux composants
#80 opened Jul 20, 2021 by florentLutz
Détailler le calcul de la masse moteur
#71 opened Jul 9, 2021 by florentLutz
Repenser le calcul de la réserve (différentes vitesses/altitudes/...)
#70 opened Jul 9, 2021 by florentLutz
Calcul du volume préssurisé
#68 opened Jul 9, 2021 by florentLutz
Diagramme V-a
#65 opened Jul 9, 2021 by florentLutz
ProTip! no:milestone will show everything without a milestone.