OpenMDAO / OpenMDAO/Aviary

Aerodynamics Code Re-Use

Open
#706 2 comments 0 reactions 4 assignees View on GitHub

@Kenneth-T-Moore is already working on this.

Since Feb 13, 2026.

code cleanup
Dominant language
Python
Stars
287
Forks
140
Avg merge
6d 14h
Merged PRs (30d)
18

Description

Desired capability or behavior.

The various aerodynamics methods have many steps in common that can likely be consolidated. The aero_common.py file is an example of a place this is happening, but it is very short (and the DynamicPressure) component should probably get moved to the Atmosphere subsystem).

A incomplete list of code that can likely be consolidated include:

  1. Scaling of aero coefficients using all of the various scaling factors provided (and using this component for all methods)
  2. Calculation of aircraft-level forces (i.e. total lift and drag) from coefficients
  3. Tabular aero (probably not all of the code, but hopefully large portions of it)
Is your feature request related to a problem? Please describe.

No response

Associated Bug Report

No response

Contributor guide

No contributing guide indexed for this repository

First steps

  1. Read the whole issue, then the project's contributing guide.
  2. Comment on the issue to say you are picking it up — it saves two people doing the same work.
  3. Fork the repository and make your change on a branch.
  4. Open a pull request that references the issue number.

Assessment

This issue has not been assessed yet.

Get new issues in your inbox

A short digest of beginner-friendly GitHub issues.