Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers

LIU Peiqing; LYU Changhao; HU Tianxiang; QU Qiulin; GENG Xin; SUN Tao

doi:10.7638/kqdlxxb-2023.0054

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Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers

更新时间：2026-05-28

- Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers
- Vol. 41, Issue 10, Pages: 100-125(2023)
- 作者机构：
  
  北京航空航天大学航空气动声学工信部重点实验室,北京,100191
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0054
  CLC： V211.44
- Published：2023
- 稿件说明：
移动端阅览
刘沛清, 吕昌昊, 胡天翔, 等. 共轴对转螺旋桨气动与噪声特性研究进展[J]. 空气动力学学报, 2023, 41(10): 100−125.

LIU Peiqing, LYU Changhao, HU Tianxiang, et al. Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers[J]. 2023, 41(10): 100-125.
刘沛清, 吕昌昊, 胡天翔, 等. 共轴对转螺旋桨气动与噪声特性研究进展[J]. 空气动力学学报, 2023, 41(10): 100−125. DOI： 10.7638/kqdlxxb-2023.0054

LIU Peiqing, LYU Changhao, HU Tianxiang, et al. Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers[J]. 2023, 41(10): 100-125. DOI： 10.7638/kqdlxxb-2023.0054.

摘要

共轴对转螺旋桨由于拉力大、气动效率高而备受人们的关注。本文从共轴对转螺旋桨的试验研究、气动性能评估、气动模拟、气动噪声预测、气动噪声优化设计等方面进行了综述。首先，总结了目前国内外在共轴对转螺旋桨气动及噪声方面的试验成果；随后，介绍了共轴对转螺旋桨气动力计算的工程方法，并详细阐述了北京航空航天大学陆士嘉实验室提出的共轴对转螺旋桨气动力评估的片条理论发展与参数选择；然后，介绍了共轴对转螺旋桨数值模拟方法，并针对共轴对转螺旋桨气动噪声预测的频域方法和时域方法进行了论述；最后，介绍了目前共轴对转螺旋桨气动噪声优化设计的研究成果。

Abstract

Counter rotating propellers (CRPs) have recently attracted more attention due to their high thrust and aerodynamic efficiency. This article comprehensively reviews five aspects of coaxial CRPs: experimental research

aerodynamic performance evaluation

aerodynamic simulation

aeroacoustics prediction

and aerodynamic noise optimization design. Firstly

it summarizes the current domestic and international experimental achievements regarding the aerodynamics and aeroacoustics of CRPs. Next

it introduces the engineering methods for the aerodynamic force calculation of CRPs and elaborates on the strip theory developed by Lu Shijia Laboratory at Beihang University for the aerodynamic force evaluation of CRPs. Based on this

numerical simulation methods for CRPs are presented

and both frequency domain and time domain methods for predicting the aerodynamic noise of CRPs are discussed. Finally

it presents the current research achievements in the aerodynamic noise optimization design of CRPs.

关键词

Keywords

references

刘沛清. 空气螺旋桨理论及其应用[M]. 北京: 北京航空航天大学出版社, 2006.

谭正平. C-130“大力神”运输机[J]. 环球军事, 2001, (10): 43.

陈宁, 李元龙. A400M: 面向未来的大型运输机[J]. 国防科技工业, 2010, (4): 58-61.

PEAKE N, PARRY A B. Modern challenges facing turbomachinery aeroacoustics[J]. Annual Review of Fluid Mechanics, 2012, 44: 227-248. DOI: 10.1146/annurev-fluid-120710-101231

ROHRBACH C, METZGER F. The prop-fan-a new look in propulsors[C]//11th Propulsion Conference, Anaheim, CA, U. S. A. , 1975. doi: 10.2514/6.1975-1208

周盛, 顾高墀, 潘杰元, 等. 航空螺旋桨与桨扇[M]. 北京: 国防工业出版社, 1994.

JR DUGAN J F, GATZEN B S, ADAMSON W M. Prop-fan propulsion - Its status and potential[R]. SAE PAPER 780995, 1978.

M'BENGUE L. Toward ACARE 2020: Innovative engine architectures to achieve the environmental goals? [C ] // 27th International Congress of the Aeronautical Sciences, Nice, France, 2010. https://www.icas.org/ICAS_ARCHIVE/ICAS2010/PAPERS/080.PDF

NEGULESCU C A. Airbus AI-PX7 CROR design features and aerodynamics[J]. SAE International Journal of Aerospace, 2013, 6(2): 626-642. DOI: 10.4271/2013-01-2245

BIERMANN D, GRAY W H. Wind-tunnel tests of eight-blade single-and dual-rotating propellers in the traction position[R ] . NACA-WR-L-384, 1941. https://digital.library.unt.edu/ark:/67531/metadc62171/m2/1/high_res_d/19930093332.pdf

GRAY W H. Wind-tunnel tests of single and dual-rotating tractor propellers at low blade angles and of two-and three-blade tractor propellers at blade angles up to 65 degrees[R ] . NACA-WR-L-316 , 1943. https://ntrs.nasa.gov/api/citations/19930093336/downloads/19930093336.pdf

HUGHES C, GAZZANIGA J. Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations[C]//24th Joint Propulsion Conference, Boston, MA, USA. Reston, Virigina: AIAA, 1988. doi: 10.2514/6.1988-3149

JR BARTLETT W A. Wind-tunnel tests of a dual-rotating propeller having one component locked or windmilling[R ] . NACA-WR-L-214, 1945. https://ntrs.nasa.gov/api/citations/19930093339/downloads/19930093339.pdf

徐传宝, 李聪, 李盛文, 等. 高雷诺数螺旋桨动力模拟风洞试验技术[C]//2019年全国工业流体力学会议, 2019.

XU Y, LI C, LI S W, et al. Experimental study on wind tunnel measurement of propeller force of turboprop aircraft[J]. Journal of Heilongjiang University of Science and Technology, 2020, 30(2): 150-154. (in Chinese)

WEI C H, JIAO L R, TONG F, et al. Pressure field measurements on large-scale propeller blades using pressure-sensitive paint[J]. Acta Mechanica Sinica, 2022, 38(2): 121366. DOI: 10.1007/s10409-021-09048-1

TANG Z H, LIU P Q, CHEN Y X, et al. Experimental study of counter-rotating propellers for high-altitude airships[J]. Journal of Propulsion and Power, 2015, 31(5): 1491-1496. DOI: 10.2514/1.b35746

DAVENPORT F, COLEHOUR J, SOKHEY J. Analysis of counter-rotating propeller performance[C]//23rd Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virigina: AIAA, 1985. doi: 10.2514/6.1985-5

PLAYLE S C, KORKAN K D, VON LAVANTE E. A numerical method for the design and analysis of counter-rotating propellers[J]. Journal of Propulsion and Power, 1986, 2(1): 57-63. DOI: 10.2514/3.22845

MAGLIOZZI B. Noise characteristics of model counter-rotating Prop-Fans[C]//11th Aeroacoustics Conference, Sunnyvale, CA, USA. Reston, Virigina: AIAA, 1987. doi: 10.2514/6.1987-2656

Block P J W. Experimental study of the effects of installation on single-and counter-rotation propeller noise[R ] . NASA-TP-2541, 1986. https://ntrs.nasa.gov/api/citations/19860016690/downloads/19860016690.pdf

WOODWARD R. Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)[C]//11th Aeroacoustics Conference, Sunnyvale, CA, USA. Reston, Virigina: AIAA, 1987. doi: 10.2514/6.1987-2657

WOODWARD R, HALL D, PODBOY G, et al. Takeoff/approach noise for a model counterrotation propeller with a forward-swept upstream rotor[C]//31st Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virigina: AIAA, 1993. doi: 10.2514/6.1993-596

RICOUARD J, JULLIARD E, REGNIER V, et al. Installation effects on contra-rotating open rotor noise[C]//16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden, 2010. doi: 10.2514/6.2010-3795

HORVÁTH C, ENVIA E, PODBOY G G. Limitations of phased array beamforming in open rotor noise source imaging[J]. AIAA Journal, 2014, 52(8): 1810-1817. DOI: 10.2514/1.j052952

PARRY A B, CRIGHTON D G. Asymptotic theory of propeller noise. I - Subsonic single-rotation propeller[J]. AIAA Journal, 1989, 27(9): 1184-1190. DOI: 10.2514/3.10244

HORVÁTH C. Beamforming investigation of dominant counter-rotating open rotor tonal and broadband noise sources[J]. AIAA Journal, 2015, 53(6): 1602-1611.

HORVÁTH C, FENYVESI B, KOCSIS B, et al. Towards counter-rotating open rotor noise reduction via radiation efficiency considerations[C]//25th AIAA/CEAS Aeroacoustics Conference, Delft, The Netherlands, 2019. doi: 10.2514/6.2019-2548

LI X D, SUN X F, HU Z. Aeroacoustical modification of a propeller[J]. Journal of Aerospace Power, 1991, 6(4): 317-319, 375 (in Chinese).

项松, 杨凤田, 吴江, 等. 某型两叶螺旋桨的设计及风洞试验[J]. 飞行力学, 2019, 37(2): 83-91.

ZHOU J J, HAO X, FU Z L, et al. Noise tests of pusher-propeller[J]. Journal of Aerospace Power, 2021, 36(2): 225-232. (in Chinese)

孙韬. 共轴对转螺旋桨气动噪声干涉特性研究[D]. 北京: 北京航空航天大学, 2022.

VAN KUIK G A M, SØRENSEN J N, OKULOV V L. Rotor theories by Professor Joukowsky: momentum theories[J]. Progress in Aerospace Sciences, 2015, 73: 1-18. DOI: 10.1016/j.paerosci.2014.10.001

GLAUERT H. The elements of aerofoil and airscrew theory[M]. 2nd ed. New York: Cambridge University Press, 1983.

OKULOV V L, SØRENSEN J N, WOOD D H. The rotor theories by Professor Joukowsky: Vortex theories[J]. Progress in Aerospace Sciences, 2015, 73: 19-46. DOI: 10.1016/j.paerosci.2014.10.002

GLAUERT H. Airplane propellers[M]//Aerodynamic Theory. Berlin, Heidelberg: Springer Berlin Heidelberg, 1935: 169-360. doi: 10.1007/978-3-642-91487-4_3

葛劳渥. 螺旋桨理论[M]. 北京: 新华印刷厂北京第一厂, 1950.

LOCK C N H. Interference velocity for a close pair of contra-rotating airscrews[R ] . ARC-RM-2084, 1941. https://reports.aerade.cranfield.ac.uk/bitstream/handle/1826.2/3432/arc-rm-2084.pdf?sequence=1isAllowed=y

GOLDSTEIN S. On the vortex theory of screw propellers[J]. Proceedings of the Royal Society of London Series A, Containing Papers of a Mathematical and Physical Character, 1929, 123(792): 440-465. DOI: 10.1098/rspa.1929.0078

NAIMAN I. Method of calculating performance of dual-rotating propellers from airfoil characteristics[R ] . NACA-WR-L-330, NACA-ARR-3E24 , 1943. https://ntrs.nasa.gov/api/citations/19930093322/downloads/19930093322.pdf

PAGE G S, LIEBECK R H. Analysis and design of dual-rotation propellers[C]//7th Applied Aerodynamics Conference, Seattle, WA, U. S. A. , 1989. doi: 10.2514/6.1989-22161989

唐智浩. 平流层飞艇共轴对转螺旋桨气动性能实验研究[D]. 北京: 北京航空航天大学, 2016.

SAITO S, KOBAYASHI H, NAKAMURA Y. Extension of local circulation method to counter rotation propeller[C]//23rd Joint Propulsion Conference, San Diego, CA, USA. Reston, Virigina: AIAA, 1987. doi: 10.2514/6.1987-1891

PETERS A, SPAKOVSZKY Z S. Rotor interaction noise in counter-rotating propfan propulsion systems[J]. Journal of Turbomachinery, 2012, 134(1): 1. DOI: 10.1115/1.4003223

HOFFER P A, DECONINCK T, HIRSCH C, et al. Aeroacoustic computations of contra-rotating open rotors using the nonlinear harmonic method and a chorochronic approach[C]// Proceedings of ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation, 2012: 217-227. doi: 10.1115/GT2012-68982

REN S L, LIU P Q. Numerical study on adjustment of the main flow field with guide vanes in transition zone for an S-duct[J]. Advances in Mechanical Engineering, 2022, 14(2): 168781402110734. doi: 10.1177/16878140211073420

SRINIVASAN G R, BAEDER J D, OBAYASHI S, et al. Flowfield of a lifting rotor in hover - A Navier-Stokes simulation[J]. AIAA Journal, 1992, 30(10): 2371-2378. DOI: 10.2514/3.11236

HILDEBRANDT T, THIEL P, ALBERT S, et al. Applying an extended non linear harmonic method to a CROR configuration with emphasis on the acoustic signature[C]//Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Volume 2A: Turbomachinery, Düsseldorf, Germany, 2014. doi: 10.1115/GT2014-25061

XU H Y, YE Z Y, SHI A M. Numerical study of propeller slipstream based on unstructured dynamic overset grids[J]. Journal of Aircraft, 2012, 49(2): 384-389. DOI: 10.2514/1.c031097

BREHM C, BARAD M F, KIRIS C C. Development of immersed boundary computational aeroacoustic prediction capabilities for open-rotor noise[J]. Journal of Computational Physics, 2019, 388: 690-716. DOI: 10.1016/j.jcp.2019.02.011

BURGGRAF U, KUNTZ M, SCHÖNING B. Implementation of the Chimera method in the unstructured DLR finite volume code TAU[M]//NITSCHE W, HEINEMANN H J, HILBIG R, eds. New results in numerical and experimental fluid mechanics II: notes on numerical fluid mechanics (NNFM), vol 72. Vieweg+Teubner Verlag, Wiesbaden, 1999. doi: 10.1007/978-3-663-10901-3_13

MADRANE A, RAICHLE A, STUERMER A. Parallel implemetation of a dynamic unstructured chimera method in the DLR finite volume TAU-code[C]//12th Annual Conference of the CFD Society of Canada (CFD 2004), 2004: 524-534.

XU H Y, YE Z. Numerical simulation of unsteady propeller slipstream[J]. Journal of Aerospace Power, 2011, 26(1): 148-153. (in Chinese)

QIAO Y H, MA D L, LI Z. Unsteady numerical simulation of propeller/wing interaction[J]. Journal of Aerospace Power, 2015, 30(6): 1366-1373. (in Chinese)

GONG X Q, MA M S, ZHANG J, et al. Unsteady numerical simulation of propeller slipstream based on unstructured chimera grid[J]. Journal of Aerospace Power, 2018, 33(2): 345-354. (in Chinese)

STOKKERMANS T C A, VAN ARNHEM N, SINNIGE T, et al. Validation and comparison of RANS propeller modeling methods for tip-mounted applications[J]. AIAA Journal, 2019, 57(2): 566-580. DOI: 10.2514/1.j057398

GEROLYMOS G A, HANISCH C. Multistage three-dimensional Navier-Stokes computation of off-design operation of a four-stage turbine[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 1999, 213(4): 243-261. DOI: 10.1243/0957650991537590

GEROLYMOS G A, TSANGA G, VALLET I. Near-wall k-ε computation of transonic turbomachinery flows with tip clearance[J ] . AIAA Journal, 1998, 36(10): 1769-1777. DOI: 10.2514/2.275

SCHNELL R, YIN J, VOSS C, et al. Assessment and optimization of the aerodynamic and acoustic characteristics of a counter rotating open rotor[J]. Journal of Turbomachinery, 2012, 134(6): 1. DOI: 10.1115/1.4006285

DELATTRE G, FALISSARD F. Influence of torque ratio on counter-rotating open-rotor interaction noise[J]. AIAA Journal, 2015, 53(9): 2726-2738. DOI: 10.2514/1.j053797

GEROLYMOS G A, MICHON G J, NEUBAUER J. Analysis and application of chorochronic periodicity in turbomachinery rotor/stator interaction computations[J]. Journal of Propulsion and Power, 2002, 18(6): 1139-1152. DOI: 10.2514/2.6065

STUERMER A. Unsteady CFD simulations of contra-rotating propeller propulsion systems[C]//44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Hartford, CT. Reston, Virigina: AIAA, 2008. doi: 10.2514/6.2008-5218

XIA Z F, YANG Y. Characteristic analysis of unsteady aerodynamic interactions of contra rotating open rotor[J]. Journal of Aerospace Power, 2014, 29(4): 835-843. (in Chinese)

黄嘉伟. 共轴高速直升机旋翼/机身/尾推气动干扰特性研究[D]. 南京: 南京航空航天大学, 2019.

SHI W B, LI J, YANG Z, et al. CFD analysis of contrarotating open rotor aerodynamic interactions[J]. International Journal of Aerospace Engineering, 2018, 2018: 1-13. DOI: 10.1155/2018/9538787

LI Z D;CHEN X X;WU T, et al. Flow characteristics and pitch regulation of high-efficiency swept-curved counter rotating propellers[J]. Journal of Aerospace Power, 2022, (8): 1703-1713.

HOUSMAN J A, KIRIS C C. Structured overlapping grid simulations of contra-rotating open rotor noise[C]//54th AIAA Aerospace Sciences Meeting, San Diego, California, USA. Reston, Virginia: AIAA, 2016. doi: 10.2514/6.2016-0814

FIORE M, DAROUKH M, MONTAGNAC M. Broadband noise prediction of a counter rotating open rotor based on LES simulation with phase-lagged assumption (draft)[J]. Journal of Sound and Vibration, 2021, 514: 116420. DOI: 10.1016/j.jsv.2021.116420

LIGHTHILL M J. On sound generated aerodynamically I. General theory[J]. Proceedings of the Royal Society of London Series A Mathematical and Physical Sciences, 1952, 211(1107): 564-587. DOI: 10.1098/rspa. 1952.0060https://royalsocietypublishing.org/doi/epdf/10.1098/rspa.1952.0060

FFOWCS WILLIAMS J E, HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transactions of the Royal Society of London Series A, Mathematical and Physical Sciences, 1969, 264(1151): 321-342. DOI: 10.1098/rsta.1969.0031

DI FRANCESCANTONIO P. A new boundary integral formulation for the prediction of sound radiation[J]. Journal of Sound and Vibration, 1997, 202(4): 491-509. DOI: 10.1006/jsvi.1996.0843

COLIN Y, CARAZO A, CARUELLE B, et al. Computational strategy for predicting CROR noise at low-speed Part I: review of the numerical methods[C]//18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), Colorado Springs, CO, 2012. doi: 10.2514/6.2012-2221

COLIN Y, BLANC F, CARUELLE B, et al. Computational strategy for predicting CROR noise at low-speed Part II: investigation of the noise sources computation with the chorochronic method[C]//18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), Colorado Springs, CO. Reston, Virigina: AIAA, 2012. doi: 10.2514/6.2012-2222

HANSON D B. Helicoidal surface theory for harmonic noise of propellers in the far field[J]. AIAA Journal, 1980, 18(10): 1213-1220. DOI: 10.2514/3.50873

HANSON D B. Noise of counter-rotation propellers[J]. Journal of Aircraft, 1985, 22(7): 609-617. DOI: 10.2514/3.45173

PARRY A B, CRIGHTON D G. Prediction of counter-rotation propeller noise[C]// 12th Aeroacoustic Conference, San Antonio, TX, U. S. A. , 1989. doi: 10.2514/6.1989-1141

KINGAN M J, PARRY A B. Time-domain analysis of contra-rotating propeller noise: wake interaction with a downstream propeller blade[J]. Journal of Fluid Mechanics, 2020, 901: A21. DOI: 10.1017/jfm.2020.504

KINGAN M J, PARRY A B. Acoustic theory of the many-bladed contra-rotating propeller: the effects of sweep on noise enhancement and reduction[J]. Journal of Sound and Vibration, 2020, 468: 115089. DOI: 10.1016/j.jsv.2019.115089

KINGAN M J, PARRY A B. Acoustic theory of the many-bladed contra-rotating propeller: analysis of the effects of blade sweep on wake interaction noise[J]. Journal of Fluid Mechanics, 2019, 868: 385-427. DOI: 10.1017/jfm.2019.172

魏宗智. 大型飞机共轴对转螺旋桨气动噪声工程预测与实验研究[D]. 北京: 北京航空航天大学, 2020.

FARASSAT F. Derivation of formulations 1 and 1A of farassat[R ] . NASA/TM-2007-214853, 2007. https://ntrs.nasa.gov/api/citations/20070010579/downloads/20070010579.pdf

PAGANO A, BARBARINO M, CASALINO D, et al. Tonal and broadband noise calculations for aeroacoustic optimization of a pusher propeller[J]. Journal of Aircraft, 2010, 47(3): 835-848. DOI: 10.2514/1.45315

VAN ZANTE D E, ENVIA E. Prediction of the aero-acoustic performance of open rotors[C]//Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany, 2014. doi: 10.1115/GT2014-26413

GIAUQUE A, ORTUN B, RODRIGUEZ B, et al. Numerical error analysis with application to transonic propeller aeroacoustics[J]. Computers Fluids, 2012, 69: 20-34. DOI: 10.1016/j.compfluid.2012.07.022

SUN X F, HU Z G, ZHOU S. Unsteady loading noise of counter-rotating propeller[J]. Journal of Aerospace Power, 1988, 3(3): 227-230, 283. (in Chinese)

JIN H B, CHEN X L, QIN X G. Open-rotor engine noise analysis based on Mohring acoustic analogy[J]. Journal of Aerospace Power, 2018, 33(4): 785-791. (in Chinese)

CUI P W, TONG F, FENG H Y, et al. Influence of rear rotor diameter on aerodynamic and acoustic characteristics of counter-rotating proeller[J]. Journal of Aerospace Power, 2022, 37(8): 1749-1760. (in Chinese)

SHU W J, CHEN C C, DU L, et al. Interaction tonal noise generated by contra-rotating open rotors[J]. Chinese Journal of Aeronautics, 2023, 36(4): 134-147. DOI: 10.1016/j.cja.2022.11.020

LI X M, LEUNG R C K, SO R M C. One-step aeroacoustics simulation using lattice Boltzmann method[J]. AIAA Journal, 2006, 44(1): 78-89. DOI: 10.2514/1.15993

QIAN Y H, D'HUMIÈRES D, LALLEMAND P. Lattice BGK models for navier-stokes equation[J]. Europhysics Letters (EPL), 1992, 17(6): 479-484. DOI: 10.1209/0295-5075/17/6/001

MARIÉ S, RICOT D, SAGAUT P. Comparison between lattice Boltzmann method and Navier-Stokes high order schemes for computational aeroacoustics[J]. Journal of Computational Physics, 2009, 228(4): 1056-1070. DOI: 10.1016/j.jcp.2008.10.021

MANOHA E, CARUELLE B. Summary of the LAGOON solutions from the benchmark problems for airframe noise computations-III workshop[C]//21st AIAA/CEAS Aeroacoustics Conference, Dallas, TX. Reston, Virginia: AIAA, 2015. doi: 10.2514/6.2015-2846

ZHANG R Y, SUN C H, LI Y B, et al. Lattice Boltzmann approach for local reference frames[J]. Communications in Computational Physics, 2011, 9(5): 1193-1205. DOI: 10.4208/cicp.021109.111110s

CHEN H, FILIPPOVA O, HOCH J, et al. Grid refinement in lattice Boltzmann methods based on volumetric formulation[J]. Physica A: Statistical Mechanics and Its Applications, 2006, 362(1): 158-167. DOI: 10.1016/j.physa.2005.09.036

CHEN H D, TEIXEIRA C, MOLVIG K. Realization of fluid boundary conditions via discrete Boltzmann dynamics[J]. International Journal of Modern Physics C, 1998, 9(8): 1281-1292. DOI: 10.1142/s0129183198001151

FARES E, WESSELS M, ZHANG R Y, et al. Validation of a lattice-Boltzmann approach for transonic and supersonic flow simulations[C]//52nd Aerospace Sciences Meeting, National Harbor, Maryland, 2014. doi: 10.2514/6.2014-0952

KÖNIG B, FARES E. Validation of a transonic lattice-Boltzmann method on the NASA common research model[C]//54th AIAA Aerospace Sciences Meeting, San Diego, California, USA. Reston, Virginia: AIAA, 2016. doi: 10.2514/6.2016-2023

CASALINO D, GRANDE E, ROMANI G, et al. Definition of a benchmark for low Reynolds number propeller aeroacoustics[J]. Aerospace Science and Technology, 2021, 113: 106707. DOI: 10.1016/j.ast.2021.106707

TERUNA C, REGO L, CASALINO D, et al. A numerical study on aircraft noise mitigation using porous stator concepts[J]. Aerospace, 2022, 9(2): 70. DOI: 10.3390/aerospace9020070

ROMANI G, GRANDE E, AVALLONE F, et al. Performance and noise prediction of low-Reynolds number propellers using the Lattice-Boltzmann method[J]. Aerospace Science and Technology, 2022, 125: 107086. DOI: 10.1016/j.ast.2021.107086

CASALINO D, GRANDE E, ROMANI G, et al. Towards the definition of a benchmark for low Reynolds number propeller aeroacoustics[J]. Journal of Physics: Conference Series, 2021, 1909(1): 012013. DOI: 10.1088/1742-6596/1909/1/012013

LYU C H, LIU P Q, HU T X, et al. A sliding mesh approach to the Lattice Boltzmann Method based on non-equilibrium extrapolation and its application in rotor flow simulation[J]. Aerospace Science and Technology, 2022, 128: 107755. DOI: 10.1016/j.ast.2022.107755

LYU C H, LIU P Q, HU T X, et al. Hybrid method for wall local refinement in lattice Boltzmann method simulation[J]. Physics of Fluids, 2023, 35(1): 017103. DOI: 10.1063/5.0130467

SMITH D A, FILIPPONE A, BARAKOS G N. Noise source analysis in counter-rotating open rotors[J]. AIAA Journal, 2022, 60(3): 1783-1796. DOI: 10.2514/1.j060886

BETZ A. The theory of the screw propeller[R ] . NACA-TN-83, 1922. https://ntrs.nasa.gov/api/citations/19930080854/downloads/19930080854.pdf

WANG J, ZHENG Y, CHEN J J, et al. Single/two-objective aerodynamic shape optimization by a Stackelberg/adjoint method[J]. Engineering Optimization, 2020, 52(5): 753-776. DOI: 10.1080/0305215x.2019.1618287

JAMESON A. Aerodynamic design via control theory[J]. Journal of Scientific Computing, 1988, 3(3): 233-260. DOI: 10.1007/BF01061285

NOCEDAL J, WRIGHT S J. Numerical optimization[M]//Springer Series in Operations Research and Financial Engineering (ORFE), 1999. doi: 10.1007/978-0-387-40065-5

KIRKPATRICK S, GELATT JR C D, VECCHI M P. Optimization by simulated annealing[J]. Science, 1983, 220(4598): 671-680. DOI: 10.1126/science.220.4598.671

KENNEDY J, EBERHART R C. Particle swarm optimization[C]//IEEE International Conference on Neural Networks, Vol. 4. IEEE service center, Piscataway, NJ, 1995: 1942-1948.

DORIGO M, MANIEZZO V, COLORNI A. Ant system: optimization by a colony of cooperating agents[J]. IEEE Transactions on Systems, Man, and Cybernetics, Part B (Cybernetics), 1996, 26(1): 29-41. DOI: 10.1109/3477.484436

GREFENSTETTE J J. Introduction[M]//Genetic Algorithms for Machine Learning. Boston, MA: Springer US, 1993: 1-4. doi: 10.1007/978-1-4615-2740-4_1

MENDOZA J. Propeller design by numerical optimization[R]// SAE Transactions, Section 3: 770404–770718, 1977, 86: 1962-1975. SAE paper 770451. doi: 10.4271/770451

PAN J Y, QIAN H D. Aerodynamic design of propeller by numerical optimization[J]. Journal of Aerospace Power, 1991, 6(4): 300-304, 374.

GUR O, ROSEN A. Multidisciplinary design optimization of a quiet propeller[C]//14th AIAA/CEAS Aeroacoustics Conference, 29th AIAA Aeroacoustics Conference, Vancouver, British Columbia, Canada, 2008. doi: 10.2514/6.2008-3073

MARINUS B, ROGER M, VAN DEN BRAEMBUSSCHE R. Aeroacoustic and aerodynamic optimization of aircraft propeller blades[C]//16th AIAA/CEAS Aeroacoustics Conference, Stockholm, Sweden. Reston, Virigina: AIAA, 2010. doi: 10.2514/6.2010-3850

MARRETTA R M A, ORLANDO C, CARLEY M. Adaptive BEM for low noise propeller design[J]. The Open Acoustics Journal, 2009, 2(1): 20-30. DOI: 10.2174/1874837600902010020

YU P X, PENG J H, BAI J Q, et al. Aeroacoustic and aerodynamic optimization of propeller blades[J]. Chinese Journal of Aeronautics, 2020, 33(3): 826-839.

WANG K L, ZHOU Z, FAN Z Y, et al. Aerodynamic design of tractor propeller for high-performance distributed electric propulsion aircraft[J]. Chinese Journal of Aeronautics, 2021, 34(10): 20-35. DOI: 10.1016/j.cja.2021.01.008

MIAN H H, WANG G, ZHOU H, et al. Optimization of thin electric propeller using physics-based surrogate model with space mapping[J]. Aerospace Science and Technology, 2021, 111: 106563. DOI: 10.1016/j.ast.2021.106563

GENG X, LIU P Q, HU T X, et al. Multi-fidelity optimization of a quiet propeller based on deep deterministic policy gradient and transfer learning[J]. Aerospace Science and Technology, 2023, 137: 108288. DOI: 10.1016/j.ast.2023.108288

STÜRMER A, AKKERMANS R D. Multidisciplinary analysis of CROR propulsion systems: DLR activities in the JTI SFWA project[J]. CEAS Aeronautical Journal, 2014, 5(3): 265-277. DOI: 10.1007/s13272-014-0105-4

GRASSO G, MOREAU S, CHRISTOPHE J, et al. Multi-disciplinary optimization of a contra-rotating fan[J]. International Journal of Aeroacoustics, 2018, 17(6-8): 655-686. DOI: 10.1177/1475472x18789000

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