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Hi, it's Matthew. Thank you again for updating your wrapper. Unfortunately, the new version has a lot of errors on my side. These seem to be general syntax (at least from what CodeBlocks outputs). Her…
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Need to understand if the RPM or Torque or both are low. - Applying torque control in region II to maximize power (peak CP). Need to match appropriate RPM when run rigid - look back at published pap…
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After running
`pip3 install .`
the pack appears to have installed successfully with output:
`Processing /Users/zach/Repos/xrotor-python`
` Installing build dependencies ... done`
` Getting …
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Hey!
During certain calculations, the results are showing 'None' return.
`xf.find_coefficients(airfoil = 'naca0012', alpha = 25, Reynolds = 1e6, iteration = 100)`
`{'alpha': None, 'CL': None, …
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1. Visualizations:
rgl, plot2D plot3D
2.CFD: export data to/ call Xfoil
call Su2/OpenFOAM?
import from SimScale results
export mesh to other CFDs
3.Correction formulae package: ...Corr
4.…
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- [ ] Case description (see #12)
- [ ] Verification and solver settings selection
- [x] Foil data comparison
- [ ] Background on the Sheldahl data
- [x] Perf curves with Sheldahl data and LB DS model
…
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Opino que no vendría mal dotar al repositorio de un módulo de herramientas.
He estado mirando, y salvo ejemplos aislados, no he encontrado ninguna biblioteca formal python para algoritmos genéticos. …
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## Bug Description / Observed Behavior
When adding a deflected control surface (flap) to an Airfoil object, the resulting geometry / coordinates have more of an abrupt curvature discontinuity than Xf…
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I have a new simulation that is not moving on from printing "Timestep: 1" after it loads the geometry and generates matrices. I didn't note my start time, but I'd say it's been there at least an hour …
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Hi,
I want to model a blade consist of 2 different Air-foil section and a transient part between two Sections.
I don't have the aerodynamic characteristics table (Cl , Cd ) of the transient part So I …