Open Access
Issue
JNWPU
Volume 40, Number 4, August 2022
Page(s) 778 - 786
DOI https://doi.org/10.1051/jnwpu/20224040778
Published online 30 September 2022
  1. ZHANG Xiaowei. Distributed electric propulsion technology oriented to 2030[C]//The 2nd China Aeronautical Science and Technology Conference, Beijing, 2015: 330-334 (in Chinese) [Google Scholar]
  2. HUANG Jun, YANG Fengtian. Development and challenges of electric aircraft with new energies[J]. Acta Aeronautica et Astronautica Sinica, 37(1): 57–68 [Article] (in Chinese) [Google Scholar]
  3. QIAO Weiyang. Aero-engine aeroacoustics[M]. Beijing: Beihang University Press, 2010 (in Chinese) [Google Scholar]
  4. XIN Gongzheng, DING Enbao, TANG Denghai. A design method for contra-rotating propeller by lifting-surface method[J]. Journal of Ship Mechanics, 2006, 10(2): 40–46 [Article] (in Chinese) [Google Scholar]
  5. LIU Xiaolong, TANG Denghai, HOU Ying. Prediction of steady performance of contra-rotating propellers by potential based panel method[J]. Shipbuilding of China, 2009, 50(3): 1–8 [Article] (in Chinese) [Google Scholar]
  6. KINNAS S. A nonlinear boundary element method for the analysis of unsteady propeller sheet cavitation[C]//Nineteenth Symposium on Naval Hydrodynamics, Seoul, Korea, 1992: 717-737 [Google Scholar]
  7. BALTAZAR J, CAMPOS J A C F D, BOSSCHERS J. Open-water thrust and torque predictions of a ducted propeller system with a panel method[J]. International Journal of Rotating Machinery, 2012(1): 474785 [Google Scholar]
  8. LEONARD A. Vortex methods for flow simulation[J]. Journal of Computational Physics, 1980, 37(3): 289–335 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  9. ANDERSON C, GREENGARD C. On vortex methods[J]. SIAM Journal on Numerical Analysis, 1985, 22(3): 413–440 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  10. TAN Jianfeng, WANG Haowen, WU Chao, et al. Rotor/empennage unsteady aerodynamic interaction with unsteady panel/viscous vortex particle hybrid method[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3): 643–656 [Article] (in Chinese) [Google Scholar]
  11. WILLIS D J, PERAIRE J, WHITE J K. A combined pFFT-multipole tree code, unsteady panel method with vortex particle wakes[J]. International Journal for Numerical Methods in Fluids, 2010, 53(8): 1399–1422 [Google Scholar]
  12. HU Hao, SONG Xiaoyong, GU Bo, et al. Aerodynamic calculation of wind turbine wheel based on hybrid panel viscous-vortex particle method[J]. Journal of Aerospace Power, 2015, 30(6): 1432–1439 [Article] (in Chinese) [Google Scholar]
  13. ZOU Ruhong, ZHANG Junyan, SUN Qin, et al. Inverse design for wind turbine airfoil based on panel method[J]. Engineering Mechanics, 2014, 31(11): 198–203 [Article] (in Chinese) [Google Scholar]
  14. BARBA L A. Vortex method for computing high-Reynolds number flows: increased accuracy with a fully mesh-less formulation[D]. Pasadena: California Institute of Technology, 2004 [Google Scholar]
  15. FENG Jianhu, NIE Yufeng, WANG Zhenhai. Numerical analysis[M]. Xi’an: Northwestern Polytechnical University Press, 2006 (in Chinese) [Google Scholar]
  16. PLOUMHANS P, WINCKELMANS G S, SALMON J K, et al. Vortex methods for direct numerical simulation of three-dimensional buff body flows: application to the sphere at Re=300, 500, and 1 000[J]. Journal of Computational Physics, 2002, 178(2): 427–463 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  17. LOWSON M. Theoretical studies of compressor noise[M]. Washington: National Aeronautics and Space Administration, 1969 [Google Scholar]
  18. KHELLADI S, KOUIDRI S, BAKIR F, et al. Predicting tonal noise from a high rotational speed centrifugal fan[J]. Journal of Sound and Vibration, 2008, 313(1): 113–133 [NASA ADS] [CrossRef] [Google Scholar]
  19. ZHAO Yinyu. Research on helicopter rotor blade-vortexinteraction noise based on coupling CFD/viscous vortex particle method[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2018 (in Chinese) [Google Scholar]
  20. DOU Fengxiang. Research on prediction for propeller non-cavitating noise[D]. Harbin: Harbin Engineering University, 2013 (in Chinese) [Google Scholar]

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