GPU-Accelerated CABARET Simulations of Distributed Propulsion for UAM

GPU-Accelerated CABARET Simulations of Distributed Propulsion for UAM

Hussain A. ABID, Igor SOLNTSEV, Andrea RAPISARDA, Hassan A. ABID, Sergey A. KARABASOV, E. DE PAOLA, Luana Georgiana STOICA, Giorgia CAPOBIANCHI, Alessandro DI MARCO, R. CAMUSSI

Abstract. Urban Air Mobility (UAM) vehicles rely on distributed propulsion (DP) to achieve efficiency, control authority, and compact integration with lifting surfaces. The close spacing of multiple rotors, however, intensifies installation effects that elevate tonal and broadband noise. This work presents a high-fidelity Large Eddy Simulation (LES) study using the CABARET method on rotating meshes to quantify aeroacoustic and aerodynamic sensitivities of a three-propeller DP configuration. The campaign varies: (i) central-rotor axial position (∆x = {-0.2Db,0,+0.2Db}), (ii) inter-rotor phase angle (0°,45°,90°,135°), and(iii) blade trailing-edge geometry (baseline vs. sawtooth serrations). Band-limited overall sound pressure level (BL OASPL) is evaluated on a probe plane under the array between the 1st and 6th blade-passing frequencies. Key findings are: (a) serrations consistently reduce area-averaged and maximum BL OASPL by up to 2.4 dB, most notably around 90◦ phase; (b) moving the central rotor closer to the wing increases thrust coefficient by ≈ 7.8%, indicating a beneficial rotor–wing interaction akin to ground effect; (c) the aerodynamic penalty of serrations is modest and attributable to effective area loss near the tip. Flow visualizations show serrations disrupt spanwise coherence and trailing-edge vortex organization, explaining the observed acoustic benefits. The results highlight the importance of joint optimization of geometry and phasing to deliver quieter, efficient DP systems for UAM.

Keywords
Distributed Propulsion, Urban Air Mobility, CABARET Method, Large Eddy Simulation, Rotating Meshes, Aeroacoustics, Trailing-Edge Serrations

Published online 7/20/2026, 7 pages
Copyright © 2026 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA

Citation: Hussain A. ABID, Igor SOLNTSEV, Andrea RAPISARDA, Hassan A. ABID, Sergey A. KARABASOV, E. DE PAOLA, Luana Georgiana STOICA, Giorgia CAPOBIANCHI, Alessandro DI MARCO, R. CAMUSSI, GPU-Accelerated CABARET Simulations of Distributed Propulsion for UAM, Materials Research Proceedings, Vol. 69, pp 564-570, 2026

DOI: https://doi.org/10.21741/9781644904251-101

The article was published as article 101 of the book CEAS – AIDAA Conference 2025

Content from this work may be used under the terms of the Creative Commons Attribution 3.0 license. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.

References
[1] Nicholas K Borer, Michael D Patterson, Jeffrey K Viken, Mark D Moore, Joe Ben Bevirt, Alex M Stoll, and Andrew R Gibson. Design and performance of the NASA sector distributed electric propulsion flight demonstrator. In 16th AIAA aviation technology, integration, and operations conference, page 3920, 2016. https://doi.org/10.2514/6.2016-3920
[2] Jean Hermetz, Michael Ridel, and Carsten Doll. Distributed electric propulsion for small business aircraft a concept-plane for key-technologies investigations. In ICAS 2016, 2016.
[3] Reynard de Vries, Nando van Arnhem, Tomas Sinnige, Roelof Vos, and Leo L. M. Veld-huis. Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight. Aerospace Science and Technology, 118:107009, 2021. https://doi.org/10.1016/j.ast.2021.107009
[4] Michael D Patterson, Joseph M Derlaga, and Nicholas K Borer. High-lift propeller system configuration selection for NASA’s sector distributed electric propulsion flight demonstrator. In 16th AIAA aviation technology, integration, and operations conference, page 3922, 2016. https://doi.org/10.2514/6.2016-3922
[5] Hyun D. Kim, Aaron T. Perry, and Phillip J. Ansell. A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology.
[6] Tian Zhou and Rami Fattah. Tonal noise acoustic interaction characteristics of multi-rotor vehicles. In 23rd AIAA/CEAS Aeroacoustics Conference, page 4054, 2017. https://doi.org/10.2514/6.2017-4054
[7] J. Thauvin, Guillaume Barraud, Marc Budinger, Xavier Roboam, Dimitri Leray, and Bruno Sareni. Hybrid regional aircraft: A comparative review of new potentials enabled by electric power. In 52nd AIAA/SAE/ASEE joint propulsion conference, page 4612, 2016. https://doi.org/10.2514/6.2016-4612
[8] J. E. Barker, A. Zarri, J. Christophe, and C. F. Schram. Numerical investigation of tonal noise emissions from propeller-wing aerodynamic and acoustic interactions. In AIAA Aviation 2023 Forum, 2023. https://doi.org/10.2514/6.2023-4056
[9] Tomas Sinnige, Nando van Arnhem, Tom C. A. Stokkermans, Georg Eitelberg, and Leo L. M. Veldhuis. Wingtip-mounted propellers: Aerodynamic analysis of interaction effects and comparison with conventional layout. Journal of Aircraft, 56(1):295-312, 2019. https://doi.org/10.2514/1.C034978
[10] Andrea Zarri, Athanasios Koutsoukos, and Francesco Avallone. Aerodynamic and acoustic interaction effects of adjacent propellers in forward flight. In 29th AIAA/CEAS Aeroacoustics Conference, page 4489, 2023. https://doi.org/10.2514/6.2023-4489
[11] Z. Yang, M. Meinke, and W. Schroder. Numerical analysis of propeller-airfoil interaction in a distributed propulsion system using a hybrid les and fw-h approach. In AIAA Aviation Forum, page 3211, 2024. https://doi.org/10.2514/6.2024-3211
[12] M. S. Howe. Aerodynamic noise of a serrated trailing edge. Journal of Fluids and Structures, 5(1):33-45, 1991. https://doi.org/10.1016/0889-9746(91)80010-B
[13] M. S. Howe. Noise produced by a sawtooth trailing edge. The Journal of the Acoustical Society of America, 90(1):482-487, 1991. https://doi.org/10.1121/1.401273
[14] M. Gruber. Airfoil noise reduction by edge treatments. PhD thesis, University of Southampton, 2012.
[15] B. Lyu, M. Azarpeyvand, and S. Sinayoko. Prediction of noise from serrated trailing edges. Journal of Fluid Mechanics, 793:556-588, 2016. https://doi.org/10.1017/jfm.2016.132
[16] T. P. Chong and A. Vathylakis. On the aeroacoustic and flow structures developed on a flat plate with a serrated sawtooth trailing edge. Journal of Sound and Vibration, 354:65-90, 2015. https://doi.org/10.1016/j.jsv.2015.05.019
[17] C. Arce-Leo’n, R. Merino-Mart’ınez, D. Ragni, F. Avallone, and M. Snellen. Boundary layer characterization and acoustic measurements of flow-aligned trailing edge serrations. Experiments in Fluids, 57(182), 2016. https://doi.org/10.1007/s00348-016-2272-z
[18] T. P. Chong, P. F. Joseph, and M. Gruber. Airfoil self-noise reduction by non-flat plate type trailing edge serrations. Applied Acoustics, 74(4):607-613, 2013. https://doi.org/10.1016/j.apacoust.2012.11.003
[19] I. Solntsev, A Chintagunta, A Markesteijn, and S Karabasov. Cabaret on rotating meshes. Elsevier Applied Mathematics and Computation, 2023. https://doi.org/10.1016/j.amc.2023.127871
[20] Anton P. Markesteijn and Sergey A. Karabasov. Cabaret solutions on graphics processing units for NASA jets: Grid sensitivity and unsteady inflow condition effect. Comptes Rendos M’ecanique, 346(10):948-963, 2018. Jet noise modelling and control Modelisation et controle du bruit de jet. https://doi.org/10.1016/j.crme.2018.07.004
[21] Vasily A. Semiletov and Sergey A. Karabasov. A volume integral implementation of the Goldstein generalized acoustic analogy for unsteady flow simulations. Journal of Fluid Mechanics, 853:461-487, 2018. https://doi.org/10.1017/jfm.2018.572
[22] Georgy A. Faranosov, Vasily M. Goloviznin, Sergey A. Karabasov, Vasily G. Kondakov, Victor F. Kopiev, and Mihail A. Zaitsev. Cabaret method on unstructured hexahedral grids for jet noise computation. Computers and Fluids, 88:165-179, 2013. https://doi.org/10.1016/j.compfluid.2013.08.011
[23] V.A. Semiletov and S.A. Karabasov. Cabaret scheme for computational aero acoustics: Extension to asynchronous time stepping and 3d flow modelling. International Journal of Aeroacoustics, 13(3-4):321-336, 2014. https://doi.org/10.1260/1475-472X.13.3-4.321
[24] Hussain Ali Abid, Sergey A. Karabasov, Annabel P. Markesteijn, and Igor Solntsev. Numerical investigation of propeller boundary layer ingestion noise using cabaret on rotating meshes. In 30th AIAA/CEAS Aeroacoustics Conference, Rome, Italy, June 2024.
[25] Weicheng Ning, Shaohong Jia, Hongyu Wang, Zhe Chen, and Bing Yang. An experimental study on small UAV propellers with serrated trailing edges. AIAA Journal, 2017. UAV-scale tests showed 0.9-1.6dB noise reduction. https://doi.org/10.2514/6.2017-3813
[26] Weicheng Xue et al. An experimental study of noise reduction in wind turbine airfoils with serrated trailing edges. arXiv preprint arXiv:2307.12188, 2023. Sawtooth serrations reduced noise by 2.7-3.0dB with thrust preservation.
[27] A. Rapisarda, L. Sangiuliano, L. D’Alessandro, and N. M. Pugno, Bio-inspired rotor designs: enhancing thrust, energy efficiency, and noise reduction,’ Bioinspiration & Biomimetics, Nov. 28, 2025. https://doi.org/10.1088/1748-3190/adf6f8
[28] B. Lyu, Mahdi Azarpeyvand, and Samuel Sinayoko. Prediction of noise from serrated trailing-edges. Journal of Fluid Mechanics, 793:1-29, 2016. Analytical model predicts noise reduction up to 10dB at 90°. https://doi.org/10.1017/jfm.2016.132
[29] D. J. Moreau and C. J. Doolan. Noise-reduction mechanism of a flat-plate serrated trailing edge. AIAA Journal, 51(10):2513-2524, 2013. https://doi.org/10.2514/1.J052436
[30] Samuel Sinayoko, B. Lyu, and M. Azarpeyvand. Prediction of noise from serrated trailing-edges (AIAA 2015). AIAA/CEAS Aeroacoustics Conference, 2015. Provided advanced analytical model validating serration performance.
[31] F. Avallone, W. C. P. Van der Velden, D. Ragni, and D. Casalino, Noise reduction mechanisms of sawtooth and combed-sawtooth trailing-edge serrations. Journal of Fluid Mechanics, 848:560-591, 2018. Confirmed geometry- and phase-dependent trends. https://doi.org/10.1017/jfm.2018.377
[32] Emanuele De Paola, Andrea Di Marco, Laurentiu G. Stoica, Luca Falcini, and Roberto Camussi. Experimental investigation on a side-by-side twin rotor system in pusher configuration. In INTER-NOISE and NOISE-CON Congress and Conference Proceedings, volume 265, pages 5862-5872, 2023. https://doi.org/10.3397/IN_2022_0870