Simulated In-Flight Wing Structural Dynamics Dataset

These data represent the structural dynamics of a wing in flight, simulated using the LltBeam simulator (GitHub). LLTBeam is a fast and efficient simulator for computing the dynamic structural response of a wing subjected to aerodynamic loads. It combines: - Lifting-line theory (LLT) to compute spanwise aerodynamic forces - An Euler–Bernoulli beam finite element model (FEM) with a cantilever configuration to simulate structural dynamics Aerodynamic loads are derived from flight conditions and projected onto the structural model, which is then integrated over time using the Newmark scheme. The framework supports time-domain simulations of flexible wings under a wide range of flight scenarios. The `flight_data` folder contains raw flight information used to compute the aerodynamic loads. It includes extensive data, some of which may not be used in the simulations. The `simulation_results` folder contains simulation outputs for each flight. These form the core dataset for training or analysis purposes. Each file includes both the structural dynamic responses and the corresponding flight conditions used during the simulation. Finally, the `simulation_and_wing_characteristics` folder contains metadata related to wing properties and simulation parameters. This dataset was generated using the `run/run.py` script in the LLTBeam repository, together with the wing definitions found in the `wing_data` folder.