| Citation: | CAO Yi-hua. Method for Predicting Rotor Vortex Wake and Downwash Velocity Field[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(2): 174-177. (in Chinese)
|
|
[1] Gray R B. Vortex modeling for rotor aerodynamics[J]. Journal of American Helicopter Society, 1992, 37(1):8~10. [2]Landgrebe A J. The wake geometry of a hovering helicopter rotor and its influence on rotor performance[J]. Journal of American Helicopter Society, 1972, 17(4):3~15. [3]Felker F F,Quackenbush T R,Bliss D B, et al. Comparisons of predicted and measured rotor performance in hover using a new free wake analysis[J]. Vertica, 1990, 14(3):361~383. [4]Lamb H. Hydrodynamics[M]. New York:Dover Publications, 1945.210~241. [5]Samant S S, Gray R B. A semi-empirical correction for the vortex core effect on hovering rotor wake geometries. In:Proceedings of 33rd Annual Forum of American Helicopter Society. Washington D C:American Helicopter Society,1977. [6]Gray R B, Brown G W. A vortex wake analysis of a single-bladed hovering rotor and a comparison with experimental data. AGARD-Cp-111, 1972. [7]Favier D,Mba M N,Barbi C, et al. A free wake analysis for hovering rotors and advancing propellers[J]. Vertica, 1987, 11(3):493~511.
|
| [1] | LI Y J，LIU Q，LI W. Impeller fault diagnosis method and application based on digital twin flow field contour of centrifugal pump[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：193-201 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0997. |
| [2] | BAI Jianfeng, MENG Junhui, ZHANG Lili, WEI Shechun, MA Nuo. Dynamic performances research of the wing deployment considering fluid structure interaction[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0645 |
| [3] | LIU Zengxu, YU Kaikai, FU Kexin, LIN Rou, XU Jinglei. Design and flow characteristics research of exhaust systems with wide altitude and speed ranges[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0781 |
| [4] | YU Rui, WANG Xiaojun, HE Xiaoying, LI Biao. Simulation and analysis of ignition flow field in granular propellant gas generators[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0683 |
| [5] | WANG Dequan, ZHAO Yuxuan, YUAN Xiangyue, WANG Qingchun, CHEN Zhongjia. Design and simulation of large composite material curing furnace based on flow field uniformity[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0370 |
| [6] | WANG Xiaoliang, WANG Congsheng, SHI Yuxiang, HE Weikun. The Classification Method of Multirotor Drones and Flying Birds under Low Signal-to-Noise Ratio for Radar[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0585 |
| [7] | LIU S S，LEI X R，SONG Z Y，et al. Influence of unloading groove opening of port plate of plunger pumps on transient flow field characteristics[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2919-2929 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0713. |
| [8] | SONG W，WANG Q，HE G Y. Visual calculation method of wing slipstream zone area on tiltrotor aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2492-2502 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0676. |
| [9] | YANG Yisong, LI Jianbo, DUAN Dengyan. Dynamic model of high confidence tilt-hinge rotor based on Newton-Euler recurrence method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0230 |
| [10] | YAN H B，XU W B，HUANG L E. Design of quadrotor attitude controller based on improved ADRC[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3283-3292 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0129. |
| [11] | GUO J J，QI J T，WANG M M，et al. A cooperative search and encirclement algorithm for quadrotors in unknown areas[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：2001-2010 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0606. |
| [12] | TANG Z Y，MA F Y，PEI Z C. Improved PSO-RBF neural network adaptive sliding mode control for quadrotor systems[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1563-1572 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0477. |
| [13] | SU D C，WANG Z Z，WU L H，et al. Flight characteristics of coaxial-rigid-rotor helicopter during deck landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：832-841 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0358. |
| [14] | WANG Zhen, ZHONG Wei, WANG Tong-guang, LI Xu-dong, ZHANG Hong-ying. Numerical simulation of unsteady aerodynamic characteristics of parafoil airfoil[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0184 |
| [15] | SHI Y，WAN Z Q，WU Z G，et al. Aerodynamic order reduction method for elastic aircraft flight dynamics simulation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1689-1706 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0510. |
| [16] | CHENG Yi, ZHAO Jin-rui, HUANG Shui-lin, YU Zhi-hao, DENG Xu-dong. Research on dynamic characteristics of distributed multi-rotor/tilting wing aeroelastic coupling[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0253 |
| [17] | WANG L N，LIU Z B，YUAN J B，et al. Adaptive fault diagnosis and estimation for quadrotor UAV[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2395-2405 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0656. |
| [18] | YANG K L，HAN D. Influence of rotor/wing aerodynamic interference on performance of compound helicopters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1761-1771 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0561. |
| [19] | WU X J，HAN X R，WU X L，et al. Prescribed performance control for quadrotor UAV with unknown kinetic parameters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2587-2595 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0714. |
| [20] | WENG Huiyan, CAI Guobiao, ZHENG Hongru, LIU Lihui, ZHANG Baiyi, HE Bijiao. Numerical simulation of effect of background pressure on electric propulsion plume field[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1854-1862. doi: 10.13700/j.bh.1001-5965.2021.0039 |
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
Yao Shuzhen, Jin Maozhong. Strategy of state transition in UML based on Petri net[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(01): 79-83. (in Chinese)
DownLoad: