Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (18): 229904.doi: 10.7527/S1000-6893.2023.29904
• Solid Mechanics and Vehicle Conceptual Design • Previous Articles
Hualong WANG, Xiayang ZHANG, Guoqing ZHAO, Qijun ZHAO(), Li MA
Received:
2023-11-27
Revised:
2023-12-28
Accepted:
2024-03-15
Online:
2024-03-22
Published:
2024-03-22
Contact:
Qijun ZHAO
E-mail:zhaoqijun@nuaa.edu.cn
Supported by:
CLC Number:
Hualong WANG, Xiayang ZHANG, Guoqing ZHAO, Qijun ZHAO, Li MA. High⁃precision simulation of aeroelastic characteristics of TEF rotor based on CFD/CSD coupling[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(18): 229904.
Table 3
Structural parameters of Fulton rotor
分段编号 | 起止位置/mm | 质量密度/(kg·m) | 挥舞惯量/(g·m) | 摆振惯量/(g·m) | 拉伸刚度/(N·m) | 扭转刚度/(N·m) | 挥舞刚度/(N·m) | 摆振刚度/(N·m) |
---|---|---|---|---|---|---|---|---|
1 | [120.64,243.32) | 4.452 5 | 0.011 1 | 0.210 9 | 43 936 347.41 | 176.93 | 332.25 | 1 858.4 |
2 | [243.32,359.87) | 7.692 5 | 0.187 9 | 3.573 3 | 8 497 582.341 | 353.86 | 445.04 | 3 709.8 |
3 | [359.87,786.92) | 5.027 8 | 0.184 6 | 3.514 2 | 11 965 451.72 | 170.41 | 252.42 | 8 550.2 |
4 | [786.92,927.58) | 11.162 | 0.239 8 | 4.558 6 | 11 424 185.11 | 121.89 | 353.31 | 4 557.8 |
5 | [927.58,1 143.0] | 4.776 4 | 0.168 2 | 3.205 5 | 12 462 529.02 | 170.41 | 252.42 | 8 550.2 |
1 | SHERIDAN P F, SMITH R P. Interactional aerodynamics:A new challenge to helicopter technology[J]. Journal of the American Helicopter Society, 1980, 25(1): 3-21. |
2 | GU Z Q. Study of control concept of adaptive rotor for vibration control: DLR 131-96/34.14S[R]. Braunschweig: DLR, 1996: 1-14. |
3 | ROTH D, ENENKL B, DIETERICH O. Active rotor control by flaps for vibration reduction: Full scale demonstrator and first flight test results[C]∥ 32nd European Rotorcraft Forum. Red Hook: Curran Associates Inc., 2007: 801-814. |
4 | MILGRAM J, CHOPRA I, STRAUB F. Rotors with trailing edge flaps: Analysis and comparison with experimental data[J]. Journal of the American Helicopter Society, 1998, 43(4): 319-332. |
5 | FRIEDMANN P P, DE TERLIZZI M, MYRTLE T F. New developments in vibration reduction with actively controlled trailing edge flaps[J]. Mathematical and Computer Modelling, 2001, 33(10/11): 1055-1083. |
6 | SHEN J W, CHOPRA I. Swashplateless helicopter rotor with trailing-edge flaps[J]. Journal of Aircraft, 2004, 41(2): 208-214. |
7 | LIM I G, LEE I. Aeroelastic analysis of rotor systems using trailing edge flaps[J]. Journal of Sound and Vibration, 2009, 321(3/4/5): 525-536. |
8 | DALLI U, YÜKSEL Ş. Identification of flap motion parameters for vibration reduction in helicopter rotors with multiple active trailing edge flaps[J]. Shock and Vibration, 2011, 18(5): 727-745. |
9 | GENNARETTI M, BERNARDINI G, SERAFINI J, et al. Helicopter vibratory loads alleviation through combined action of trailing-edge flap and variable-stiffness devices[J]. International Journal of Aerospace Engineering, 2015, 2015: 485964. |
10 | JAIN R, YEO H, CHOPRA I. Computational fluid dynamics: Computational structural dynamics analysis of active control of helicopter rotor for performance improvement[J]. Journal of the American Helicopter Society, 2010, 55(4): 042004. |
11 | 王荣, 夏品奇. 多片后缘小翼对直升机旋翼桨叶动态失速及桨毂振动载荷的控制[J]. 航空学报, 2013, 34(5): 1083-1091. |
WANG R, XIA P Q. Control of helicopter rotor blade dynamic stall and hub vibration loads by multiple trailing edge flaps[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(5): 1083-1091 (in Chinese). | |
12 | LIU S M, YANG W D, WU J. Study on vibratory loads of rotor with trailing edge excitation[J]. Advanced Materials Research, 2014, 1044/1045: 877-880. |
13 | 周桓. 基于双后缘小翼的智能旋翼振动抑制及实现研究[D]. 南京: 南京航空航天大学, 2020: 29-35. |
ZHOU H. Research on vibration suppression and realization of smart rotor based on dual trailing-edge flaps[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020: 29-35 (in Chinese). | |
14 | SU T Y, LU Y, MA J C, et al. Aerodynamic characteristics analysis of electrically controlled rotor based on viscous vortex particle method[J]. Aerospace Science and Technology, 2020, 97: 105645. |
15 | SHEN J W, CHOPRA I. Aeroelastic stability of trailing-edge flap helicopter rotors[J]. Journal of the American Helicopter Society, 2003, 48(4): 236-243. |
16 | 刘士明, 杨卫东, 虞志浩, 等. 后缘小翼智能旋翼减振效果影响因素分析[J]. 振动与冲击, 2017, 36(3): 138-144. |
LIU S M, YANG W D, YU Z H, et al. Influence factors analysis for smart vibration control of a rotor wing with trailing edge flaps[J]. Journal of Vibration and Shock, 2017, 36(3): 138-144 (in Chinese). | |
17 | 关晓辉, 李占科, 宋笔锋. CST气动外形参数化方法研究[J]. 航空学报, 2012, 33(4): 625-633. |
GUAN X H, LI Z K, SONG B F. A study on CST aerodynamic shape parameterization method[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(4): 625-633 (in Chinese). | |
18 | 马奕扬, 招启军, 赵国庆. 基于后缘小翼的旋翼翼型动态失速控制分析[J]. 航空学报, 2017, 38(3): 120312. |
MA Y Y, ZHAO Q J, ZHAO G Q. Dynamic stall control of rotor airfoil via trailing-edge flap[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(3): 120312 (in Chinese). | |
19 | 马奕扬, 招启军. 后缘小翼对旋翼气动特性的控制机理及参数分析[J]. 航空学报, 2018, 39(5): 121671. |
MA Y Y, ZHAO Q J. Control mechanism and parameter analyses of aerodynamic characteristics of rotor via trailing-edge flap[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(5): 121671 (in Chinese). | |
20 | 招启军, 徐国华. 直升机计算流体动力学基础[M]. 北京: 科学出版社, 2016: 62-67. |
ZHAO Q J, XU G H. Foundations of helicopter computational fluid dynamics[M]. Beijing: Science Press, 2016: 62-67 (in Chinese). | |
21 | 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. |
22 | 周金龙, 董凌华, 杨卫东, 等. 基于加权最小二乘法辨识的后缘襟翼智能旋翼振动载荷闭环控制仿真研究[J]. 振动与冲击, 2019, 38(4): 237-244. |
ZHOU J L, DONG L H, YANG W D, et al. Closed-loop vibration control simulation of a helicopter active rotor with trailing-edge flaps based on the weighted-least-squares-error identification method[J]. Journal of Vibration and Shock, 2019, 38(4): 237-244 (in Chinese). | |
23 | ZHOU Z X, HUANG X C, TIAN J J, et al. Numerical and experimental analysis on the helicopter rotor dynamic load controlled by the actively trailing edge flap[J]. Smart Material Structures, 2022, 31(3): 035023. |
24 | 周子宣, 田嘉劲, 唐敏, 等. 主动后缘襟翼对旋翼桨毂振动载荷控制的机理与风洞试验[J]. 机械工程学报, 2023, 59(14): 254-263. |
ZHOU Z X, TIAN J J, TANG M, et al. Mechanism and wind tunnel experiment of active controlled flap on vibration load control of rotor hub[J]. Journal of Mechanical Engineering, 2023, 59(14): 254-263 (in Chinese). | |
25 | YUAN K A, FRIEDMANN P P. Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips: NASA-CR-4665[R]. Washington, D.C.: NASA, 1995. |
26 | ZHANG X Y, WANG H L, ZHAO Q J, et al. Structural modeling and dynamic analysis of the two-segment deployable beam system[J]. International Journal of Mechanical Sciences, 2022, 233: 107633. |
27 | ZHANG X Y, CHEN X, ZHANG K, et al. Structural modeling and modal analysis of rotor blade during ice accretion[J]. Aerospace Science and Technology, 2022, 123: 107448. |
28 | NEWMARK N M. A method of computation for structural dynamics[J]. Journal of the Engineering Mechanics Division, 1959, 85(3): 67-94. |
29 | 赵蒙蒙. 基于CFD/CSD耦合方法的复合材料旋翼结构载荷优化分析[D]. 南京: 南京航空航天大学, 2017: 12-13. |
ZHAO M M. Optimization analyses on structural load of composite rotor based on CFD/CSD coupling method[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017: 12-13 (in Chinese). | |
30 | HEFFERNAN R M, GAUBERT M. Structural and aerodynamic loads and performance measurements of an SA349/2 helicopter with an advanced geometry rotor: NASA-TM-88370[R]. Washington, D. C.: NASA, 1986. |
31 | 马砾, 招启军, 赵蒙蒙, 等. 基于CFD/CSD耦合方法的旋翼气动弹性载荷计算分析[J]. 航空学报, 2017, 38(6): 120762. |
MA L, ZHAO Q J, ZHAO M M, et al. Computation analyses of aeroelastic loads of rotor based on CFD/CSD coupling method[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(6): 120762 (in Chinese). | |
32 | 王松. 基于CFD/CSD松耦合的直升机稳态飞行状态配平与载荷预估[D]. 南京: 南京航空航天大学, 2019: 76-77. |
WANG S. Trim and load estimation of steady flight state of helicopter based on CFD/CSD loose coupling [D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2019:76-77 (in Chinese). | |
33 | ANANTHAN S, BAEDER J, SIM B W, et al. Predic-tion and validation of the aerodynamics, structure dynamics, and acoustics of the SMART rotor using a loosely-coupled CFD-CSD analysis[C]∥ 66th Annual Forum and Technology Display of the American Helicopter Society International. Alexandria: The AHS International Inc., 2010: 2031-2057. |
34 | HASSAN A A, STRAUB F K, NOONAN K W. Experimental/numerical evaluation of integral trailing edge flaps for helicopter rotor applications[J]. Journal of the American Helicopter Society, 2005, 50(1): 3-17. |
35 | FULTON M V, ORMISTON R A. Hover testing of a small-scale rotor with on-blade elevons[J]. Journal of the American Helicopter Society, 2001, 46(2): 96-106. |
36 | FULTON M V, ORMISTON R A. Small-scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight[C]∥ American Helicopter Society 54th Annual Forum. Washington, D. C.: The AHS International Inc., 1998: 1-18. |
37 | 刘士明. 带后缘小翼的智能旋翼振动载荷抑制研究[D]. 南京: 南京航空航天大学, 2016: 59-63. |
LIU S M. Research on vibratory load control of smart rotor with trailing edge flaps[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016: 59-63 (in Chinese). | |
38 | 刘士明, 杨卫东, 虞志浩, 等. 带后缘小翼的旋翼振动载荷计算[J]. 航空动力学报, 2016, 31(6): 1496-1503. |
LIU S M, YANG W D, YU Z H, et al. Vibratory loads prediction of rotor with trailing edge flaps[J]. Journal of Aerospace Power, 2016, 31(6): 1496-1503 (in Chinese). |
[1] | Guoqiang LI, Kuihui SONG, Chen QIN, Guangyin ZHAO, Linxin WU, Yongdong YANG. Test on active control of airfoil dynamic stall based on trailing edge flap [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 128699-128699. |
[2] | Songbai WANG, Yuyang HAO, Yadong WU, Yong CHEN, Huawei YU, Lin DU. Research progress on rotating instability of aeroengine compressor [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(16): 29851-029851. |
[3] | Cheng ZHANG, Haoyuan REN, Tailong SHI, Wendi DAI. Multidisciplinary full-time coupling methods of folding fin containing non-linear connections and their applications [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729461-729461. |
[4] | Shijie YU, Xinghua ZHOU, Rui HUANG. Parametric aeroelastic modeling and flutter characteristic analysis of variable camber wing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 227346-227346. |
[5] | Peihan WANG, Zhigang WU, Chao YANG, Xiaoxu SUN. Patch module method for flight simulation of flexible aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127038-127038. |
[6] | Weijia LIU, Yingkun LI, Xiong CHEN, Chunlei LI. Panel flutter characteristics on shock wave/boundary layer interaction based on fluid⁃structure coupling [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127085-127085. |
[7] | Songbai WANG, Yong CHEN, Yadong WU, Shaoping ZHANG, Zhipeng CAO. Research progress on non-synchronous vibration of axial compressor rotor blade [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(17): 28044-028044. |
[8] | Libo WANG, Zhiwei JING, Chu TANG. Modelling and simulation of flexible aircraft in blast wind [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(17): 228214-228214. |
[9] | LI Yingjie, ZHAO Guang, WU Xueshen, LI Jian, YUAN Wei, MEI Qing. Review of research on self-excited vibration of aviation spline-rotor system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 625532-625532. |
[10] | ZHOU Yitao, YANG Yang, WU Zhigang, YANG Chao. Flight test for gust alleviation on a high aspect ratio UAV platform [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526126-526126. |
[11] | YANG Chao, QIU Qisheng, ZHOU Yitao, WU Zhigang. Review of aircraft gust alleviation technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527350-527350. |
[12] | WANG Xinjiang, LIU Ziqiang, GUO Li, FU Zhichao, LYU Jinan. Analysis method for flutter mode indicator based on principle of work and power [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 224920-224920. |
[13] | SUN Yan, WANG Hao, JIANG Meng, YUE Hao, MENG Dehong. Design and implementation of coupling acceleration strategy in static aeroelastic module of NNW-FSI software [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 625738-625738. |
[14] | LI Kui, YANG Zhichun, GU Yingsong, ZHOU Shengxi. Performance enhancement of variable-potential-well bi-stable aeroelasticity energy harvesting [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 223710-223710. |
[15] | LI Qiuyan, LI Gang, WEI Yangtian, RAN Yuguo, WU Bo, TAN Guanghui, LI Yan, CHEN Shi, LEI Boqi, XU Qinwei. Review of aeroelasticity design for advanced fighter [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(6): 523430-523430. |
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