Open Access
| Issue |
JNWPU
Volume 43, Number 6, December 2025
|
|
|---|---|---|
| Page(s) | 1101 - 1109 | |
| DOI | https://doi.org/10.1051/jnwpu/20254361101 | |
| Published online | 02 February 2026 | |
- WIESNER W, KOHLER G. Tail rotor performance in presence of main rotor, ground, and winds[J]. Journal of the American Helicopter Society, 1974, 19(3): 2–9 [Article] [Google Scholar]
- DOOLAN C J, LECLERCQ D. An anechoic wind tunnel for the investigation of the main-rotor/tail-rotor blade vortex interaction[C]//Proceedings of the 6th Australian Vertiflite Conference on Helicopter Technology, Virginia, 2007 [Google Scholar]
- KAYNES I W, PREATONI G, VISINGARDI A, et al. Heliflow pitch-up and quartering flight experiments[C]//26th European Rotorcraft Forum, the Hague, the Netherlands, 2000 [Google Scholar]
- SRINIVAS V, CHOPRA I, HAAS D, et al. Prediction of tail rotor thrust and yaw control effectiveness[J]. Journal of the American Helicopter Society, 1995, 40(4): 34–43 [Article] [Google Scholar]
- QUACKENBUSH T R, BLISS D B. Prediction of high-resolution flow fields for rotorcraft aeroacoustics[J]. AIAA Journal, 1991, 29(11): 1778–1786 [Article] [Google Scholar]
- YIN Jianping, HU Zhangwei. Numerical simulation of mutual interference between helicopter main and tail rotors' free wakes[J]. Acta Aerodynamica Sinica, 1998(4): 21–25 (in Chinese) [Google Scholar]
- YIN J P, AHMED S R. Aerodynamics and aeroacoustics of helicopter main-rotor/tail-rotor interaction[C]//15th Aerodynamic Decelerator Systems Technology Conference, Reston, 1999: 1-13 [Google Scholar]
- TAN Jianfeng, WANG Haowen. Numerical analysis of unsteady aerodynamic interference of helicopter rotor/fuselage[J]. Acta Aerodynamica Sinica, 2014, 32(3): 320–327 (in Chinese) [Google Scholar]
- TAN Jianfeng. Influence of helicopter rotor on unsteady aerodynamic loads of tail rotor[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(10): 3228–3240 (in Chinese) [Google Scholar]
- RUISH Michael. Unstructured, multiplex rotor source model with thrust and moment trimming-fluent's VBM model[C]//23rd AIAA Applied Aerodynamics Conference, 2012 [Google Scholar]
- WANG C, HUANG M, MA S, et al. Main rotor wake interference effects on tail rotor thrust in crosswind[J]. International Journal of Aerospace Engineering, 2021(1): 9994115 [Google Scholar]
- YANG C, AONYAMA T, KONDON N, et al. Numerical analysis for main-rotor/tail-rotor interaction of helicopter[R]. JAXA-RR-08-006E, 2009 [Google Scholar]
- FAN Feng, XU Guohua, SHI Yongjie. Unsteady aerodynamic interference calculation of helicopter rotor/tail rotor based on CFD method[J]. Journal of Aerospace Power, 2014, 29(11): 2633–2642 (in Chinese) [Google Scholar]
- YE Zhou, XU Guohua, SHI Yongjie. Calculation of rotor/tail rotor/tail gas dynamic interference of helicopter[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9): 2874–2883 (in Chinese) [Google Scholar]
- SUN Yukun, WANG Long, WANG Tongguang, et al. Aerodynamic characteristics and crosswind resistance optimization of isolated tail rotor under crosswind[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(10): 65–81 (in Chinese) [Google Scholar]
- CHEN R T N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications[R]. NASA TM 1989-102219 [Google Scholar]
- LI Jinsheng, CHANG Sijiang, CHEN Shengfu. Projectile resistance coefficient Identification based on neural network algorithm[J]. Acta Ballistics Sinica, 2018, 30(4): 38–43 (in Chinese) [Google Scholar]
- SPRING S C, NIEMANN J R, GRADY G W. Preliminary airworthiness evaluation CH-47C with fiberglass rotor blades (with T55-L-712 engines)[EB/OL]. (2023-09-14)[2025-01-03]. http://handle.dtic.mil/100.2/ADA06989 [Google Scholar]
- WEN Long, Research on aerodynamic performance of heli copter tail rotor in main rotor interference flow field[D]. Xi'an: Northwestern Polytechnical University, 2025 (in Chinese) [Google Scholar]
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