tigl
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DLR-SC
The TiGL Geometry Library to process aircraft geometries in pre-design.
We need test for the python bindings. As at least on of the CI jobs builds the bindings, we can test them easily.
Fuselage noses and tails are often modelled using profile curves that are scaled down to a singular point. There are two problems causing errors when trying to combine zero-length profiles...
Its not an issue but I dont know the channel to get this question across. Its possible to creta an deposition ribs and spars programmatically ?
Following up #802, it has been found that the order of segment faces is wrong, if the leading edge is zero  Making shells in line https://github.com/DLR-SC/tigl/blob/1ffa6c5cbc750b843449ed66614f2489237493d4/src/geometry/CTiglPatchShell.cpp#L162 reorders the faces....
**Important Note!** : I looked at the implementation of `TrimFace`. Currently, this will only work, if the face was not trimmed before and uses more complicated face boundaries (e.g. skewed...
The two classes are conceptually very similar and it makes sense to refactor them into one. What `CTiglCompoundSurface` adds to `CTiglRectSurface` is the functionality of quering points from the shape...
Currently our unit test suite contains a few performance tests using `ctime`. By seperating benchmarks from unit tests - we speed up the test suite, because benchmarks are a bit...
We use wing cells to define the material distribution on wind turbine baldes. An example dataset of a blade can be found below: [IEA-10.0-198-RWT_CPACS.xml.zip](https://github.com/DLR-SC/tigl/files/5770559/IEA-10.0-198-RWT_CPACS.xml.zip) As discussed with @joergbrech , there...
The generation of the geometries of the spars are very slow (about 15 minutes). The example consists of two spars with two segments each. [IEA-15-240-RWT_CPACS.zip](https://github.com/DLR-SC/tigl/files/5666376/IEA-15-240-RWT_CPACS.zip)