NonLinearStatic¶
Structural solver used for the static simulation of free-flying structures.
This solver provides an interface to the structural library (
xbeam) and updates the structural parameters for every k-th step of the FSI iteration.This solver can be called as part of a standalone structural simulation or as the structural solver of a coupled static aeroelastic simulation.
The settings that this solver accepts are given by a dictionary, with the following key-value pairs:
Name Type Description Default print_infoboolPrint output to screen Truemax_iterationsintSets maximum number of iterations 100num_load_stepsint1delta_curvedfloat0.01min_deltafloatStructural solver tolerance 1e-05newmark_dampfloatSets the Newmark damping coefficient 0.0001gravity_onboolFlag to include gravitational forces FalsegravityfloatGravitational acceleration 9.81relaxation_factorfloat0.3dtfloatTime step increment 0.01num_stepsint500initial_positionlist(float)<sphinx.ext.autodoc.importer._MockObject object at 0x7f8a2858e080>