Assessment of synchrophasing for a pair of rotors in close proximity

This paper investigates the aerodynamics and aeroacoustics of a pair of rotors within the “Radiation and Propagation for Multirotor Systems” project from the Group for Aeronautical Research and Technology in Europe (GARTEUR) Action Group 26. The study employs validated high-fidelity computational fluid dynamics (CFD), the in-house Helicopter Multi-Block Solver 3 (HMB3), to investigate a pair of dual-bladed 13x7 rotors in hover and edgewise flights. The study aims to reduce rotor noise by introducing a phase offset between the starting positions of the rotors in tandem configurations. The rotors maintained a constant RPM, and a tip Mach number of 0.4, close to typical values for full-scale urban air mobility (UAM) rotorcraft. Results indicated a performance loss from tandem rotors compared to isolated configurations, especially for the downstream rotor. However, the performance of the downstream rotor is slightly recovered in the tandem offset configuration. A comprehensive synchrophasing study based on cumulative effect of the rarefaction and compression in the acoustic wave is also presented, showing different levels of noise reduction without compromising performance. More than 20 dBA of noise reduction was observed in several one-third octaves bands, and up to 7 dBA of overall noise reduction was achieved at optimal de-phased cases for the region between the two rotors. In the meantime, the most beneficial phases can be adjusted to achieve maximum noise reduction at different locations, including upstream, inter-rotor, and downstream regions. Furthermore, transforming from a single isolated rotor to the optimal de-phased tandem offset configuration while producing the same amount of lift achieved almost 10 dBA noise reduction, suggesting a perceived noise that is 50% lower in reality. • High-fidelity aerodynamic and aero-acoustic modelling of propellers in edgewise flight. • Comparison of isolated propeller noise with noise from two propellers in close proximity. • Investigation of the effect of phase in the overall noise of the system.

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Publication Details

Journal
Aerospace Science and Technology
Published
2024-12-04
DOI
https://doi.org/10.1016/j.ast.2024.109808
Citations
7
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
2.62

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article

Assessment of synchrophasing for a pair of rotors in close proximity

G. Qiao, George N. Barakos, Emma San Martin
7 citations
Aerospace Science and Technology
Computational Fluid Dynamics and Aerodynamics
2.62
article

Assessment of synchrophasing for a pair of rotors in close proximity

G. Qiao, George N. Barakos, Emma San Martin
article en
7 citations

Abstract

This paper investigates the aerodynamics and aeroacoustics of a pair of rotors within the “Radiation and Propagation for Multirotor Systems” project from the Group for Aeronautical Research and Technology in Europe (GARTEUR) Action Group 26. The study employs validated high-fidelity computational fluid dynamics (CFD), the in-house Helicopter Multi-Block Solver 3 (HMB3), to investigate a pair of dual-bladed 13x7 rotors in hover and edgewise flights. The study aims to reduce rotor noise by introducing a phase offset between the starting positions of the rotors in tandem configurations. The rotors maintained a constant RPM, and a tip Mach number of 0.4, close to typical values for full-scale urban air mobility (UAM) rotorcraft. Results indicated a performance loss from tandem rotors compared to isolated configurations, especially for the downstream rotor. However, the performance of the downstream rotor is slightly recovered in the tandem offset configuration. A comprehensive synchrophasing study based on cumulative effect of the rarefaction and compression in the acoustic wave is also presented, showing different levels of noise reduction without compromising performance. More than 20 dBA of noise reduction was observed in several one-third octaves bands, and up to 7 dBA of overall noise reduction was achieved at optimal de-phased cases for the region between the two rotors. In the meantime, the most beneficial phases can be adjusted to achieve maximum noise reduction at different locations, including upstream, inter-rotor, and downstream regions. Furthermore, transforming from a single isolated rotor to the optimal de-phased tandem offset configuration while producing the same amount of lift achieved almost 10 dBA noise reduction, suggesting a perceived noise that is 50% lower in reality. • High-fidelity aerodynamic and aero-acoustic modelling of propellers in edgewise flight. • Comparison of isolated propeller noise with noise from two propellers in close proximity. • Investigation of the effect of phase in the overall noise of the system.

Aerospace Science and TechnologyVol. 157
University of Glasgow (GB)
Marshall Aid Commemoration Commission, Engineering and Physical Sciences Research Council, James Watt School of Engineering, University of Glasgow
Openalex Percentile: Top 10%
Computational Fluid Dynamics and Aerodynamics
2.62
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