Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (9): 529256-529256.doi: 10.7527/S1000-6893.2023.29256
• Articles • Previous Articles Next Articles
Zhuangzhuang CUI, Xin YUAN, Guoqing ZHAO, Simeng JING, Qijun ZHAO()
Received:
2023-07-03
Revised:
2023-09-19
Accepted:
2023-10-16
Online:
2024-05-15
Published:
2023-11-01
Contact:
Qijun ZHAO
E-mail:zhaoqijun@nuaa.edu.cn
Supported by:
CLC Number:
Zhuangzhuang CUI, Xin YUAN, Guoqing ZHAO, Simeng JING, Qijun ZHAO. Influence of control strategy on forward flight performance of coaxial rigid rotor high⁃speed helicopters[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529256-529256.
1 | CHENEY M C. The ABC helicopter[J]. Journal of the American Helicopter Society, 1969, 14(4): 10-19. |
2 | KWON Y M, PARK J S, WIE S Y, et al. Aeromechanics analyses of a modern lift-offset coaxial rotor in high-speed forward flight[J]. International Journal of Aeronautical and Space Sciences, 2021, 22(2): 338-351. |
3 | OZDEMIR G T. In-flight performance optimization for rotorcraft with redundant controls[D]. Michigan: The Pennsylvania State University, 2013: 48-49. |
4 | CAO Y H, WANG M S, LI G Z. Flight dynamics modeling, trim, stability, and controllability of coaxial compound helicopters[J]. Journal of Aerospace Engineering, 2021, 34(6): 04021084. |
5 | QIU Y Q, LI Y, LANG J X, et al. Dynamics analysis and control of coaxial high-speed helicopter in transition flight[J]. Aerospace Science and Technology, 2023, 137: 108278. |
6 | FERGUSON K, THOMSON D. Performance comparison between a conventional helicopter and compound helicopter configurations[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015, 229(13): 2441-2456. |
7 | SAITO S, AZUMA A. A numerical approach to co-axial rotor aerodynamics[C]∥Seventh European Rotorcraft and Powered Lift Aircraft Forum. Garmisch-Partenkirchen: Federal Republic of Germany, 1981. |
8 | VALKOV T V. Aerodynamic loads computation on coaxial hingeless helicopter rotors[C]∥ Proceedings of the 28th Aerospace Sciences Meeting. Reston: AIAA, 1990. |
9 | KIM H W, KENYON A R, BROWN R E, et al. Interactional aerodynamics and acoustics of a hingeless coaxial helicopter with an auxiliary propeller in forward flight[J]. The Aeronautical Journal, 2009, 113(1140): 65-78. |
10 | 佘明人. 共轴刚性旋翼高速直升机飞行动力学建模及飞行特性研究[D]. 南京: 南京航空航天大学, 2021: 11-19. |
SHE M R. Research on the flight dynamics modeling and flight characteristics of a coaxial rigid rotor high-speed helicopter[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2021: 11-19 (in Chinese). | |
11 | 张银. 复合式共轴刚性旋翼直升机气动干扰及飞行特性分析[D]. 南京: 南京航空航天大学, 2014: 47-49. |
ZHANG Y. Research on aerodynamic interaction and flight characteristics of compound helicopter with rigid coaxial rotor[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014: 47-49 (in Chinese). | |
12 | 袁野, 陈仁良, 李攀. 基于涡环尾迹模型的共轴刚性旋翼直升机飞行动力学建模[J]. 航空学报, 2018, 39(3): 121564. |
YUAN Y, CHEN R L, LI P. Flight dynamic modelling for coaxial rigid rotor helicopter using vortex-ring wake model[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(3): 121564 (in Chinese). | |
13 | 卢丛玲, 祁浩天, 徐国华. 升力偏置对共轴刚性旋翼前飞气动特性的影响[J]. 航空学报, 2019, 40(11): 122906. |
LU C L, QI H T, XU G H. Influence of lift offset on rigid coaxial rotor aerodynamic characteristics in forward flight[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(11): 122906 (in Chinese). | |
14 | 原昕, 招启军, 朱正, 等. 前飞速度和升力偏置量对共轴刚性旋翼气动特性影响分析[J]. 南京航空航天大学学报, 2019, 51(2): 213-219. |
YUAN X, ZHAO Q J, ZHU Z, et al. Flow-field characteristics measurements of coaxial rigid rotor in forward flight[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2019, 51(2): 213-219 (in Chinese). | |
15 | HAYAMI K, SUGAWARA H, YUMINO T, et al. CFD analysis on the performance of a coaxial rotor with lift offset at high advance ratios[J]. Aerospace Science and Technology, 2023, 135: 108194. |
16 | ZHAO Q J, ZHAO G Q, WANG B, et al. Robust Navier-Stokes method for predicting unsteady flowfield and aerodynamic characteristics of helicopter rotor[J]. Chinese Journal of Aeronautics, 2018, 31(2): 214-224. |
17 | WANG B, CAO C K, ZHAO Q J, et al. Aeroacoustic characteristic analyses of coaxial rotors in hover and forward flight[J]. International Journal of Aeronautical and Space Sciences, 2021, 22(6): 1278-1292. |
18 | 招启军, 张威, 原昕, 等. 共轴刚性旋翼气动外形优化设计[J]. 南京航空航天大学学报, 2019, 51(2): 160-165. |
ZHAO Q J, ZHANG W, YUAN X, et al. Optimization design of coaxial rotor aerodynamic planform[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2019, 51(2): 160-165 (in Chinese). | |
19 | NAGASHIMA T, SHINOHARA K, BABA T. A flow visualization study for the tip vortex geometry of the coaxial counter rotating rotor in hover[J]. Technical Note, 1977, 25(284): 442-445. |
20 | COLEMAN C P. A survey of theoretical and experimental coaxial rotor aerodynamic research: NASA/TP-1997-3675[R]. Washington, D.C.: NASA, 1997. |
21 | DINGELDEIN R C. Wind-tunnel studies of the performance of multirotor configurations: NACA/TN-1954-3236[R]. Washington, D.C.: NACA, 1954. |
22 | EVANS A J, LINER G. A wind-tunnel investigation of the aerodynamic characteristics of a full-scale sweptback propeller and two related straight propellers: NACA/RM-1951-L5005[R]. Washington, D.C.: NACA, 1951. |
23 | FREEMAN C E, MINECK R E. Fuselage surface pressure measurements of a helicopter wind-tunnel model with a 3.15-meter diameter single rotor: NASA/TM-1979-80051[R]. Washington, D.C.: NASA, 1979. |
24 | WANG B, YUAN X, ZHAO Q J, et al. Geometry design of coaxial rigid rotor in high-speed forward flight[J]. International Journal of Aerospace Engineering, 2020, 2020: 6650375. |
25 | 陈仁良, 高正. 直升机飞行动力学[M]. 北京: 科学出版社, 2003: 4-8. |
CHEN R L, GAO Z. Helicopter flight dynamics[M]. Beijing: Science Press, 2003: 4-8 (in Chinese). | |
26 | JING S M, ZHAO Q J, ZHAO G Q, et al. Multi-objective airfoil optimization under unsteady-freestream dynamic stall conditions[J]. Journal of Aircraft, 2023, 60(2): 293-309. |
27 | BALLIN M. Validation of a real-time engineering simulation of the UH-60A helicopter: NASA-TM88360[R]. Washington, D.C.: NASA, 1987. |
[1] | Qi LIU, Yongjie SHI, Zhiyuan HU, Guohua XU. Parameter effects analysis on aerodynamic and aeroacoustic characteristics of coaxial rigid rotor [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 528856-528856. |
[2] | Pengpeng SUN, Ping’an LIU, Feng FAN, Wei ZENG. Aerodynamic interaction characteristics of coaxial rigid rotor⁃fuselage in hover condition [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529284-529284. |
[3] | Jiaqi LIU, Rongqian CHEN, Jinhua LOU, Xu HAN, Hao WU, Yancheng YOU. Aerodynamic shape optimization of high-speed helicopter rotor airfoil based on deep learning [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529828-529828. |
[4] | Chang WANG, Long HE, Dongxia XU, Min TANG, Shuai MA, Ximing WU. Flow control drag reduction of hub on coaxial rigid rotor aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529084-529084. |
[5] | Shaoqiang HAN, Wenping SONG, Zhonghua HAN, Jianhua XU. High-accuracy numerical-simulation of unsteady flow over high-speed coaxial rigid rotors [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529064-529064. |
[6] | Zixu WANG, Pan LI, Ke LU, Zhenhua ZHU, Renliang CHEN. Optimized design of trim strategy for coaxial rigid rotor high-speed helicopter [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529069-529069. |
[7] | Yuhan LI, Baoyu YANG, Yinong WU, Qiang ZHANG, Xiao TANG. Research on parameters correction method for thermal model of satellite optomechanical load [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 628814-628814. |
[8] | Qichang CHEN, Zhiwei SHI, Weiyuan ZHANG, Linglong YAO, Shengxiang TONG. Aerodynamic layout and control strategy design and flight verification of a wing⁃foldable variant VTOL aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629583-629583. |
[9] | Shusheng CHEN, Cong FENG, Zhaokang ZHANG, Ke ZHAO, Xinyang ZHANG, Zhenghong GAO. Aerodynamic design of wide-speed-range waverider-wing configuration based on global & gradient optimization method [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629596-629596. |
[10] | Zhenyang HAO, Ling QIN, Xin CAO, Qiyao ZHANG, Qiang ZHOU. Optimal servo system and modulation method of mechanical antenna array [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 328692-328692. |
[11] | Qian YANG, Haoran ZHENG, Xianda CHENG, Wei DONG. Optimization design method for hot air anti⁃icing system based on bleed air control [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729285-729285. |
[12] | Huan ZHAO, Zhenghong GAO, Lu XIA. Novel multi-fidelity surrogate model assisted many-objective optimization method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 126962-126962. |
[13] | Huan ZHAO, Zhenghong GAO, Lu XIA. Aerodynamic shape design optimization method based on novel high⁃dimensional surrogate model [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 126924-126924. |
[14] | Zhiyang ZHENG, Yang ZHANG, Zhao ZHANG, Baohai WU, Ying ZHANG. Layout optimization of auxiliary support for thin-walled blade based on GA-SVR [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 426805-426805. |
[15] | Xian’ang ZENG, Dongqiang ZHAO, Junjie LI, Zezhou YAN, Chengyu LIU. Wind tunnel test on gust alleviation control strategies of elastic wing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 226869-226869. |
Viewed | ||||||
Full text |
|
|||||
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341