Neural Ordinary Differential Equations for rotorcraft aerodynamics
Peter Rivera-Casillas,
Ian Dettwiller
Abstract:High-fidelity computational simulations of aerodynamics and structural dynamics on rotorcraft are essential for helicopter design, testing, and evaluation. These simulations usually entail a high computational cost even with modern high-performance computing resources. Reduced order models can significantly reduce the computational cost of simulating rotor revolutions. However, reduced order models are less accurate than traditional numerical modeling approaches, making them unsuitable for research and design … Show more
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