Enumerations | |
General TIGL handling functions | Function to open, create, and close CPACS-files |
Functions for wing calculations | Function to handle wing geometry's with TIGL |
Functions for fuselage calculations | Function to handle fuselage geometry's with TIGL |
Functions for rotor calculations | Functions to handle rotor geometries with TIGL |
Functions for rotor blade calculations | Functions to handle rotor blade geometries with TIGL |
Functions for boolean calculations | Function for boolean calculations on wings/fuselages |
Export Functions | Functions for export of wings/fuselages |
Material functions | Functions to query material information of wings/fuselages. Materials are currently ony implemented for the wing component segment. Here, materials for the lower and upper wing surface can be queried, which can be a material for the whole skin/surface or a material defined inside a wing cell. A wing cell material overwrites the global skin material, i.e. if the whole wing skin material is aluminum and the trailing edge is made of radar absorbing material, only the absorbing material is returned by the querying functions |
Functions for volume calculations | Function for volume calculations on wings/fuselages |
Functions for surface area calculations | Function for surface area calculations of wings/fuselages |
General geometry functions. | |
Logging functions. | The following functions are used to customize the behaviour how messages are handled by TiGL. By default, only error messages and warnings are printed to the console |
Generic utility functions. | Generic utility functions for geometric components that fits not only to wings or fuselages |