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The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and frequency domain as well as dynamic landing loads based on a generic landing gear module.
Aircraft design optimization made fast through modern automatic differentiation. Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
This project introduces a fault detection framework using neural networks for the RCAM. The study begins by remodeling the RCAM’s nonlinear dynamics to simulate various fault conditions. Subsequently, data generated from these faulty models underpin the training and testing of neural networks.
A great tool to ease the Calculations for Aircraft Design Project. Everything's Automated, give the required values and ADPHelper will do everything for you!