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### Description of the modifications
When trying the documentation examples that use the launch_modeler() command I get an uncaught execution when creating a new design even though the connection is …
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Single taper
- [x] import aerofoil data file
- [x] create sketch from aerofoil points
- [x] scale aerofoil
- [x] clone aerofoil to new position
- [x] add dihedral
- [x] add twist
- [x] add swee…
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Hello,
I've correctly installed your module but when I attempt to set a Mach Number, it doesn't have any effect on the calculations. The coefficients stay the same.
Here's a plot with the generated …
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Hi,
I am trying to predict the noise from a NACA 0012 airfiol, for which I have information on the pressure and force coefficients. I have set up a simulation and am getting almost identical values …
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```
What steps will reproduce the problem?
Parse a cobol array with an INDEXED BY clause containing multiple index
declaration, for example :
01 TAB OCCURS 10 INDEXED BY IDX1 IDX2 IDX3.
What is the …
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So far, the project is divided into tutorials (`src/tutorials`) and examples (`src/examples`). The tutorials all share the same `Project.toml` located at the root of the project whereas each example h…
bmxam updated
5 months ago
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csv_timeline360.py is asking for f35b_elevator.txt, which is not in folder F35B.
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### Description
It seems it's not possible to map a single container port to multiple host ports when using host mode. It might be similar to this issue: https://github.com/docker/compose-cli/issues/…
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Continuing from #9, we need to know how much `k` and `epsilon` should be injected based on the foil performance.
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# Description of feature
I'm wondering if composites laminates would be straightforward to implement in OpenAeroStruct ? Would be neat for [aeroelastic tailoring
](https://en.wikipedia.org/wiki/Aero…