-
I'd like to work toward using the C++ version of the site update program. @yakra are you confident in the threaded version's readiness for production site updates?
I think that moving to the C++ p…
-
本期打卡已结算完成。报名最新一期的打卡活动 [点这里](https://mp.weixin.qq.com/s/eUG2OOzY3k_ZTz-CFvtv5Q)
-
Hi Neks,
I am simulating flows around a NACA airfoil at Re=10^4/10^6 using the rans_komg.f module from Nek5000 (the latest updated version as reported in the article by Tomboulides et al. Int. J. H…
-
### Issue Type
- [ ] Bug
- [ ] Enhancement
### Description
Keep getting panel buckling solutions, with OML panels near the root sometimes buckling. We are still experiencing panel buckling s…
-
I think there is a minus missing in the derivative calculation in line 238 (naca5) of naca.py. Without fixing, if the number of points is too large, a discontinuity appears in the max camber location.
-
hello I am using blueCFD OpenFOAM 5.x on Windows 7.
I've conducted a simulation of flow around naca airfoil using the SA turbulence model. The simulation finished (The link to download the case is gi…
-
Hello, everyone.
I am a new user of blendyn. It looks insteresting to render MBDyn model in blender.
However, when I tried to render a rotating beam, I find the beam will rotate 360deg (eg. fro…
-
Hi,
We have been trying to figure out the reasons causing the difference in the time-averaged thrust coefficients of the NREL 5MW wind turbine obtained from wind tunnel experiments and FAST simula…
-
## dhis2
Username: admin
## Browser
- Name: Mozilla
- Version: 5.0 (Windows NT 10.0; Win64; x64) AppleWebKit/537.36 (KHTML, like Gecko) Chrome/89.0.4389.114 Safari/537.36
- Platform: Win32
## User …
-
## Bug Description
When importing `aerosandbox.library.airfoils` warnings are raised relating to the lack of coordinates available for the generic and flat plate airfoils.
## Steps to Reproduce
`…