3.2.3
Modules
Here is a list of all modules:
 Enumerations
 General TIGL handling functionsFunction to open, create, and close CPACS-files
 Functions for wing calculationsFunction to handle wing geometry's with TIGL
 Functions for fuselage calculationsFunction to handle fuselage geometry's with TIGL
 Functions for rotor calculationsFunctions to handle rotor geometries with TIGL
 Functions for rotor blade calculationsFunctions to handle rotor blade geometries with TIGL
 Functions for boolean calculationsFunction for boolean calculations on wings/fuselages
 Export FunctionsFunctions for export of wings/fuselages
 Material functionsFunctions 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 calculationsFunction for volume calculations on wings/fuselages
 Functions for surface area calculationsFunction 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