Directional noise reduction via rotor phase–shifting for multirotor aircraft

• 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.

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Publication Details

Journal
Aerospace Science and Technology
Published
2026-01-15
DOI
https://doi.org/10.1016/j.ast.2026.111699
Citations
1
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
104.69
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article

Directional noise reduction via rotor phase–shifting for multirotor aircraft

Thorsten Schwarz, Gabriele Bellani, Emanuele L. de Angelis, Jianping Yin et al.
1 citations
Aerospace Science and Technology
Aerodynamics and Acoustics in Jet Flows
104.69
article

Directional noise reduction via rotor phase–shifting for multirotor aircraft

Thorsten Schwarz, Gabriele Bellani, Emanuele L. de Angelis, Jianping Yin, Aldo Chella, Diego Donnini, Francesco Sessini
article en
1 citations

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.

Aerospace Science and TechnologyVol. 172
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR) (DE), University of Bologna (IT)
Sustainable cities and communities
Openalex Percentile: Top 1%
Aerodynamics and Acoustics in Jet Flows
104.69
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