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All issues Volume 43 / No 5 (October 2025) JNWPU, 43 5 (2025) 853-861 References
Open Access
Issue
JNWPU
Volume 43, Number 5, October 2025
Page(s) 853 - 861
DOI https://doi.org/10.1051/jnwpu/20254350853
Published online 05 December 2025
  1. PICKLES D J, ZAGAGLIA D, BUSSE A, et al. Vortex ring state of a shrouded rotor: an experimental survey[J]. Experiments in Fluids, 2023, 64(4): 69 [Article] [Google Scholar]
  2. SURMACZ K, RUCHAŁA P, STRYCZNIEWICZ W. Wind tunnel tests of the development and demise of vortex ring state of the rotor[C]//Proceedings of the 3rd Polish Congress of Mechanics and 21st International Conference on Computer Methods in Mechanics, 2015: 8-11 [Google Scholar]
  3. VEISMANN M, DOUGHERTY C, GHARIB M. Effects of rotor separation on the axial descent performance of dual-rotor configurations[J]. Flow, 2023, 3: E7 [Article] [Google Scholar]
  4. TALAEIZADEH A, ANTUNES D, PISHKENARI H N, et al. Optimal-time quadcopter descent trajectories avoiding the vortex ring and autorotation states[J]. Mechatronics, 2020, 68: 102362 [Article] [Google Scholar]
  5. WOLKOVITCH J. Analytical prediction of vortex-ring boundaries for helicopters in steep descents[J]. Journal of the American Helicopter Society, 1972, 17(3): 13–19 [Article] [Google Scholar]
  6. PETERS D A, CHEN S Y. Momentum theory, dynamic inflow, and the vortex-ring state[J]. Journal of the American Helicopter Society, 1982, 27(3): 18–24 [Article] [Google Scholar]
  7. XIN Hong, GAO Zheng. A prediction of the helicopter vortex-ring state boundary[J]. Aerodynamic Experiment and Measurement & Control, 1996, 10(1): 14–19 (in Chinese) [Google Scholar]
  8. STALEWSKI W, SURMACZ K. Investigations of the vortex ring state on a helicopter main rotor based on computational methodology using URANS solver[C]//Proceedings of 9th EASN International Conference on “Innovation in Aviation & Space”, 2019 [Google Scholar]
  9. WANG Junjie, CHEN Renliang, WANG Zhijin, et al. Numerical simulation and mathematical modeling of vortex ring state of tiltrotor aircraft[J]. Journal of Harbin Institute of Technology, 2023, 55(4): 35–43 (in Chinese) [Google Scholar]
  10. GAO Zeming, SHAO Xueming, WANG Jiading, et al. Aerodynamic characteristics and vortex ring features of propeller in vertical descent[J]. Acta Aerodynamica Sinica, 2024, 42(10): 1–11 (in Chinese) [Google Scholar]
  11. FU Weijia, MA Jingzhong, LI Jie. IDDES numerical simulation of rotor tip vortices in hovering[J]. Journal of Northwestern Polytechnical University, 2019, 37(1): 195–202 (in Chinese) [Google Scholar]
  12. WANG Gang, YE Zhengyin. Study of the unsteady flow around a delta wing at high incidence using detached eddy simulation[J]. Journal of Northwestern Polytechnical University, 2008, 26(4): 413–418 (in Chinese) [Google Scholar]
  13. LI Xu, ZHU Xiaoping, ZHOU Zhou, et al. The numerical simulation of UAV's landing in ship airwake[J]. Journal of Northwestern Polytechnical University, 2019, 37(1): 186–194 (in Chinese) [Google Scholar]
  14. SPALART P R, ALLMARAS S R. A one-equation turbulencemodel for aerodynamic flows[R]. AIAA-1992-0439, 1992 [Google Scholar]
  15. SPALART P R. Detached-eddy simulation[J]. Annual Review of Fluid Mechanics, 2009, 41: 181–202 [Article] [CrossRef] [Google Scholar]
  16. PETERSSON N A. Hole-cutting for three-dimensional overlapping grids[J]. SIAM Journal on Scientific Computing, 2006, 21(2): 646–665 [Google Scholar]
  17. MEAKIN R L. A new method for establishing intergrid communication among systems of overset grids[R]. AIAA-1991-1586, 1991 [Google Scholar]
  18. DECONINCK H, ROE P L, STRUIJS R. A multidimensional generalization of Reo's flux difference splitter for the Euler equations[J]. Computers Fluids, 1993, 22(2): 215–222 [Google Scholar]
  19. PANDYA S A, VENKATESWARAN S, PULLIAM T H. Implementation of dual-time procedures in overflow[R]. AIAA-2003-0072, 2003 [Google Scholar]
  20. HUANG Mingqi, LAN Bo, HE Long. Wind tunnel test on aerodynamic characteristics of rotor model in vertical descent[J]. Journal of Harbin Institute of Technology, 2019, 51(4): 131–137 (in Chinese) [Google Scholar]

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