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High-Fidelity Computational Analysis on the Noise of a Side-by-Side Hybrid VTOL Aircraft
This paper investigates the acoustics of a side-by-side urban air mobility (UAM) aircraft with 0%, 5%, 15%, and 25% rotor overlaps in forward flight based on high-fidelity computational fluid dynamics (CFD) simulations. The CFD and acoustics simulations are carried out using the HPCMP CREATE
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Record · ID 1119902
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