mdolab / mdolab/OpenAeroStruct
Orthotropic material
Open
Nobody has claimed this yet.
enhancement
- Dominant language
- Python
- Stars
- 281
- Forks
- 135
- PR merge metrics
- No merged PRs in 30d
Description
Description of feature
I'm wondering if composites laminates would be straightforward to implement in OpenAeroStruct ? Would be neat for aeroelastic tailoring
Potential solution
Using a non-diagonal stiffness matrix would be relatively easy I reckon.
Contributor guide
No contributing guide indexed for this repository
First steps
- Read the whole issue, then the project's contributing guide.
- Comment on the issue to say you are picking it up — it saves two people doing the same work.
- Fork the repository and make your change on a branch.
- Open a pull request that references the issue number.
Research direction
No files, tests, or entry points are named. Begin by locating the material stiffness representation in OpenAeroStruct and assess how composite laminates and a non-diagonal stiffness matrix would fit; done would require a defined implementation scope and validation for aeroelastic tailoring.
Written by the indexing model from the issue text.
Assessment
- Tech stack
- python
- Domain
- backend
- Issue type
- Feature
- Difficulty
- 5/5
- Estimated time
- Over a week
- Activity status
- Stale
- Clarity
- Needs clarification
- Newbie friendliness
- 20/100