Directional noise reduction via rotor phase–shifting for multirotor aircraft

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Authors: Francesco Sessini, Diego Donnini, Aldo Chella, Thorsten Schwarz, Jianping Yin, Gabriele Bellani, Emanuele L. de Angelis
Cited by: 2
References: 9

Abstract

• Develops a numerical toolchain framework for aeroacoustic analysis. • Investigates the effect of rotor phase shift on aeroacoustics in VTOL multirotor vehicles. • Proposes an analytical methodology for fast sound prediction, useful for hover optimization. • Develops a numerical trim methodology coupled with the aerodynamic solver to account for mutual aerodynamic interactions. • Demonstrates the effects of optimized rotor phase shift in both hover and level forward flight conditions. • Keywords: Urban Air Mobility; aeroacoustics; rotor phase synchronization; active noise reduction; VTOL. This study investigates rotor phase synchronization as a strategy for directional noise reduction in multirotor vertical take–off and landing (VTOL) aircraft employing collective pitch control. The application of this approach enables the redirection of acoustic emissions away from noise–sensitive regions without degrading aerodynamic performance or requiring alterations to the flight trajectory. A dedicated simulation framework integrates the mid–fidelity aerodynamic solver UPM with the aeroacoustic prediction model APSIM, developed at the German Aerospace Center (DLR), Institute of Aerodynamics and Flow Technology. To reproduce representative flight conditions, a trimming procedure determines the required control inputs and vehicle attitude. Such simulation methodology was validated by reproducing available experimental data for hovering fixed–pitch propellers. To identify optimal rotor phasing for noise redirection in full–scale quadrotor and hexarotor configurations under trimmed flight conditions, two distinct optimization strategies are employed. In forward flight, optimization is conducted using the complete high–fidelity simulation environment. For hover conditions, an analytical aeroacoustic model based on compact source theory provides a computationally efficient alternative that reduces the demands placed on the optimizer. Acoustic pressure evaluations on a ground plane beneath the vehicle confirm that optimized rotor phasing successfully redirects noise away from designated regions.

Fields of Study & Subjects

Aerodynamics and Acoustics in Jet Flows Computational Fluid Dynamics and Aerodynamics Lattice Boltzmann Simulation Studies

Publication details

Journal / source
Aerospace Science and Technology
Publisher
Elsevier BV
Volume
172
Pages
111699–111699
Publication date
15 January 2026
Language
EN