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Hi i was looking for it but i think that for now there is no option to to change for example boundary layer parameters for airfoil evaluation in xoptfoil-jx. (that's a pitty, because with it, the prog…
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I propose we create a 0.0 release of GPfit and then perform a pretty wholesale refactor of the code. Here is the list of changes I would like to make:
- [x] General code tightening (more concise co…
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Today I was tracking down the test failure observed in https://github.com/JuliaMath/IntelVectorMath.jl/pull/39 when moving to MKL_jll that occurred on a Mac.
After a while, with some help from @gio…
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Hi!
I was reading your eVTOL example, where you simulate a maneuver and i noticed that, for all the propellers, you read just one polar at a fixed Reynolds number. This means that the aerodynamics …
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Feature request:
Is there a way to set minimum-cp (from the xflr OpPoint view F5) as a constraint or penalty to be above a certain value (maybe for a defined AOA range)?
This can be relevant fo…
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## Description
When trying to calculate airfoil and xfoil is failing to converge, i receive error that airfoil is failing to converge and program terminates execution
I guess there is no much us…
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## Description
Develop Branch, example 07_te_flaps appears to be incapable of producing flap actuation as currently set up.
Found by:
- Plotting the FAST output (both .out and .outb) for BLFLAP…
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1.airfoil.generate_polars work well in Windows, but it can't work in Ubuntu22.04. I found it caused by Xfoil .
2. I also found there is a bug "def _run_xfoil()" in Xfoil.py ( lines 264) , In linux , …
Zcaic updated
12 months ago
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Hi,
I was trying to follow the steps described in Readme to run an example (see code below) but it throwed me the following error. Could you please help on how to solve it?
**Error**
```
Trace…
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The airfoil data can be attain by xfoil, and usually we set the chord length equal 1 in xfoil, but in the config.ini, the chord length does not equal 1, should I change the chord length in xfoil setti…