tario

Is it possible to export the Spline Parameters? Secondary but nice-to-have: Is it possible to change the number of Spline Parameters?

Hello, I installed the latest trunk version of xflr5 on RHEL9/AlmaLinux9 Linux but get an error when I try to start xflr5: xflr5: error while loading shared libraries: libXFoil.so.1: cannot open shared object file: No such file or directory But during the installation things went well - see below make[1]: Verzeichnis „/home/klaus/Programme/xflr5-code-r1431-trunk/xflr5/XFoil-lib“ wird betreten /usr/bin/qmake-qt5 -install qinstall -exe libXFoil.so.1.0.0 /usr/local/lib/libXFoil.so.1.0.0 strip --strip-unneeded...

I think I have v6.43 working, the latest version gives me a QNetworkReplyHttpImplPrivate::_q_startOperation was called more than once QUrl("https://www.xflr5.com/rss/rssfeed.xml") Speicherzugriffsfehler error. Speicherzugriffsfehler = memory access error sudo make install the individual parts made no difference.

the problem is, due to the new install locations, I get an error: ./xflr5: error while loading shared libraries: libxflr5-engine.so.1: cannot open shared object file: No such file or directory Same with the latest version.

Hello, I wanted to upgrade from version v6,41 to the latest version v6.44 on Linux but I couldn't find the v6.44 source code. Will it be available? I "tried to install" v6.43 but it's installed into new/different default locations: v6.41: /usr/bin /usr/lib64 v6.43: /usr/local/bin /usr/local/lib v6.43 doesn't start as the required libraries are not found. Where should I add or correct the path? T.

Thank you for pointing out the limitation. My problem with the VLM2 is that cl and cp predictions are incorrect, cl is too high and -cp is way too low while the 3D Panels method produces correct results for the wingbody only. My judgement is based on a validation using actual measurement data and empirical correlations. Both are in line with the results obtained with the 3D Panels method. Do you see a practical way to get an idea of the flow or pressure distribution at intersections?

Attached an example, I want to get an idea about the flow at the T-joint but xflr5 craches all the time, most of the time without even "remembering", that I defined a fin."

I'm using v6.41 and have the same problem. I work on a wing body and want to add a fin. xflr5 crashes immediately when I try to run an analysis.