Aerodynamic Modeling and Simulation of Multi-Lifting Surfaces Based on the Unsteady Vortex Lattice Method

Using the unsteady vortex lattice method based on potential flow theory, a rapid modeling approach is developed for aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid divisions can be quickly integrated meshed object-oriented data structure. The physical influence between was modeled, wake–surface interaction also considered by using built-in core models. trajectory were used to replace pre-calculated downwash superposition boundary condition integration, instantaneous generated directly from kinematic states mesh messages model concerned. Considering direct coupling effect aerodynamics rigid body dynamics, function free flight built medium-fidelity dynamic simulations identifications. proposed high-efficiency simulation process easily applied models any number arbitrary motion modes.