ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (8): 227346-227346.doi: 10.7527/S1000-6893.2022.27346
• Solid Mechanics and Vehicle Conceptual Design • Previous Articles
Shijie YU, Xinghua ZHOU, Rui HUANG()
Received:
2022-04-28
Revised:
2022-05-20
Accepted:
2022-07-13
Online:
2022-07-25
Published:
2022-07-21
Contact:
Rui HUANG
E-mail:ruihwang@nuaa.edu.cn
Supported by:
CLC Number:
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.
1 | DECAMP R W, HARDY R. Mission adaptive wing research programme[J]. Aircraft Engineering and Aerospace Technology, 1981, 53(1): 10-11. |
2 | DECAMP R, HARDY R. Mission adaptive wing advanced research concepts[C]∥ 11th Atmospheric Flight Mechanics Conference. Reston: AIAA, 1984. |
3 | BONNEMA K, SMITH S. AFTI/F-111 mission adaptive wing flight research program[C]∥ 4th Flight Test Conference. Reston: AIAA, 1988. |
4 | JHA A K, KUDVA J N. Morphing aircraft concepts, classifications, and challenges[C]∥ Smart Structures and Materials 2004: Industrial and Commercial Applications of Smart Structures Technologies, 2004, 5388: 213-224. |
5 | PASTOR C, SANDERS B, JOO J J, et al. Kinematically designed flexible skins for morphing aircraft[C]∥ Proceedings of ASME 2006 International Mechanical Engineering Congress and Exposition, 2007: 89-95. |
6 | KUDVA J N, JARDINE A P, MARTIN C A, et al. Overview of the ARPA/WL “smart structures and materials development-smart wing” contract[C]∥ Smart Structures and Materials 1996: Industrial and Commercial Applications of Smart Structures Technologies, 1996, 2721: 10-16. |
7 | KUDVA J N, APPA K, VAN WAY C B, et al. Adaptive smart wing design for military aircraft: requirements, concepts, and payoffs[C]∥ Smart Structures and Materials 1995: Industrial and Commercial Applications of Smart Structures Technologies, 1995, 2447: 35-44. |
8 | BARTLEY-CHO J D, WANG D P, MARTIN C A, et al. Development of high-rate, adaptive trailing edge control surface for the smart wing phase 2 wind tunnel model[J]. Journal of Intelligent Material Systems and Structures, 2004, 15(4): 279-291. |
9 | HETRICK J, OSBORN R, KOTA S, et al. Flight testing of mission adaptive compliant wing[C]∥ 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston: AIAA, 2007. |
10 | DI MATTEO N, GUO S J, AHMED S, et al. Design and analysis of a morphing flap structure for high lift wing[C]∥ 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston: AIAA, 2010. |
11 | CAMPANILE L F. Modal synthesis of flexible mechanisms for airfoil shape control[J]. Journal of Intelligent Material Systems and Structures, 2008, 19(7): 779-789. |
12 | SINAPIUS M, MONNER H P, KINTSCHER M, et al. DLR’s morphing wing activities within the European network[J]. Procedia IUTAM, 2014, 10: 416-426. |
13 | 王彬文, 杨宇, 钱战森, 等. 机翼变弯度技术研究进展[J]. 航空学报, 2022, 43(1): 024943. |
WANG B W, YANG Y, QIAN Z S, et al. Research progress of variable camber wing technology[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(1): 024943 (in Chinese). | |
14 | 刘世丽, 葛文杰, 李奎, 等. 基于杆索基结构的三维柔性变形机翼结构拓扑优化设计[J]. 机械科学与技术, 2008, 27(10): 1191-1194. |
LIU S L, GE W J, LI K, et al. Optimal structural design of a three-dimensional morphing aircraft wing based on strut and cable ground structure[J]. Mechanical Science and Technology for Aerospace Engineering, 2008, 27(10): 1191-1194 (in Chinese). | |
15 | 李飞. 飞机自适应机翼的驱动机构研究[D]. 南京: 南京航空航天大学, 2009. |
LI F. Research on adaptive wing structures based on NITI SMA actuator[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009 (in Chinese). | |
16 | 黄建. 新型零泊松比蜂窝结构力学性能及其变弯度机翼应用研究[D]. 哈尔滨: 哈尔滨工业大学, 2018. |
HUANG J. Mechanical performances of a novel honeycomb design with zero Poisson’s ratio and its application in camber morphing wings[D]. Harbin: Harbin Institute of Technology, 2018 (in Chinese). | |
17 | WU Y, DAI Y T, YANG C, et al. Effect of trailing-edge morphing on flow characteristics around a pitching airfoil[J]. AIAA Journal, 2021, 61(1): 160-173. |
18 | 倪迎鸽, 侯赤, 万小朋, 等. 折叠机翼的参数化气动弹性建模与颤振分析[J]. 西北工业大学学报, 2015, 33(5): 788-793. |
NI Y G, HOU C, WAN X P, et al. Parametric aeroelastic modeling and flutter analysis for a folding wing[J]. Journal of Northwestern Polytechnical University, 2015, 33(5): 788-793 (in Chinese). | |
19 | ZHAO Y H, HU H Y. Parameterized aeroelastic modeling and flutter analysis for a folding wing[J]. Journal of Sound and Vibration, 2012, 331(2): 308-324. |
20 | ZHOU X H, HUANG R. Efficient nonlinear aeroelastic analysis of a morphing wing via parameterized fictitious mode method[J]. Nonlinear Dynamics, 2021, 105(1): 1-23. |
21 | ALBANO E, RODDEN W P. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows[J]. AIAA Journal, 1969, 7(2): 279-285. |
22 | 杨宁, 吴志刚, 杨超, 等. 折叠翼的结构非线性颤振分析[J]. 工程力学, 2012, 29(2): 197-204. |
YANG N, WU Z G, YANG C, et al. Flutter analysis of a folding wing with structural nonlinearity[J]. Engineering Mechanics, 2012, 29(2): 197-204 (in Chinese). | |
23 | 刘艳. 连续变弯度后缘机翼静气动弹性分析及优化设计[D]. 西安: 西北工业大学, 2016. |
LIU Y. Aeroelasticity analysis method and optimization design for aircraft wing with variable camber continuous trailing edge[D]. Xi’an: Northwestern Polytechnical University, 2016 (in Chinese). | |
24 | 吴优, 戴玉婷, 张仁嘉, 等. 连续变弯度翼型动态气动特性数值模拟[J]. 北京航空航天大学学报, 2021, 47(6): 1241-1253. |
WU Y, DAI Y T, ZHANG R J, et al. Numerical simulation of dynamic aerodynamic characteristics of a camber morphing airfoil[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(6): 1241-1253 (in Chinese). | |
25 | ZHOU Q, CHEN G, RONCH A DA, et al. Reduced order unsteady aerodynamic model of a rigid aerofoil in gust encounters[J]. Aerospace Science and Technology, 2017, 63: 203-213. |
26 | WINTER M, HECKMEIER F M, BREITSAMTER C. CFD-based aeroelastic reduced-order modeling robust to structural parameter variations[J]. Aerospace Science and Technology, 2017, 67: 13-30. |
27 | SEBER G, BENDIKSEN O O. Nonlinear flutter calculations using finite elements in a direct Eulerian-Lagrangian formulation[J]. AIAA Journal, 2008, 46(6): 1331-1341. |
28 | LYU Z J, MARTINS J R R A. Aerodynamic design optimization studies of a blended-wing-body aircraft[J]. Journal of Aircraft, 2014, 51(5): 1604-1617. |
29 | KENWAY G K W, MARTINS J R R A. Multipoint high-fidelity aerostructural optimization of a transport aircraft configuration[J]. Journal of Aircraft, 2014, 51(1): 144-160. |
30 | 郭同彪, 白俊强, 李立, 等. 民用客机变弯度机翼优化设计[J]. 中国科学: 技术科学, 2018, 48(1): 55-66. |
GUO T B, BAI J Q, LI L, et al. The morphing trailing-edge wing optimization design of the civil aircraft[J]. Scientia Sinica (Technologica), 2018, 48(1): 55-66 (in Chinese). | |
31 | JO Y, CHOI S, ZIENTARSKI L, et al. Aerodynamic characteristics and shape optimization of a variable camber compliant wing[C]∥ 34th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2016. |
32 | 梁煜, 单肖文. 大型民机翼型变弯度气动特性分析与优化设计[J]. 航空学报, 2016, 37(3): 790-798. |
LIANG Y, SHAN X W. Aerodynamic analysis and optimization design for variable camber airfoil of civil transport jet[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3): 790-798 (in Chinese). | |
33 | 黄锐, 胡海岩. 飞行器非线性气动伺服弹性力学[J]. 力学进展, 2021, 51(3): 428-466. |
HUANG R, HU H Y. Nonlinear aeroservoelasticity of aircraft[J]. Advances in Mechanics, 2021, 51(3): 428-466 (in Chinese). | |
34 | KATZ J, PLOTKIN A. Low speed aerodynamics: From wing theory to panel methods[M]. New York: McGraw-Hill, 1991. |
35 | AMSALLEM D, CORTIAL J, CARLBERG K, et al. A method for interpolating on manifolds structural dynamics reduced-order models[J]. International Journal for Numerical Methods in Engineering, 2009, 80(9): 1241-1258. |
36 | AMSALLEM D, FARHAT C. Interpolation method for adapting reduced-order models and application to aeroelasticity[J]. AIAA Journal, 2008, 46(7): 1803-1813. |
37 | 詹玖榆, 周兴华, 黄锐. 基于流形切空间插值的折叠翼参数化气动弹性建模[J]. 力学学报, 2021, 53(4): 1103-1113. |
ZHAN J Y, ZHOU X H, HUANG R. Parametric aeroelastic modeling of folding wing based on manifold tangent space interpolation[J]. Chinese Journal of Theoretical and Applied Mechanics, 2021, 53(4): 1103-1113 (in Chinese). | |
38 | 郭同庆. 复杂组合体跨音速非定常气动力和颤振计算[D]. 南京: 南京航空航天大学, 2006. |
GUO T Q. Transonic unsteady aerodynamics and flutter computations for complex assemblies[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2006 (in Chinese). | |
39 | YAO X J, HUANG R, HU H Y. Data-driven modeling of transonic unsteady flows and efficient analysis of fluid-structure stability[J]. Journal of Fluids and Structures, 2022, 111: 103549. |
[1] | Haoyu CHEN, Binwen WANG, Qiaozhi SONG, Xiaodong LI. Thermal flutter ground simulation test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 227295-227295. |
[2] | Jiong REN, Gang WANG, Guodong HU, Xiaolu SHI. Adaptive finite volume method with Walsh basis functions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127444-127444. |
[3] | Yuanhe LIU, Kebo LI, Shaoming HE, Yangang LIANG. Flying range control guidance for varying⁃speed missiles based on optimal error dynamics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 326909-326909. |
[4] | 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. |
[5] | 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. |
[6] | Bi WEN, Baijie QIAO, Zepeng LI, Zhendong LI, Yanfeng WANG, Xuefeng CHEN. Synchronous vibration identification of fan blisk based on acoustic mode decomposition [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 227066-227066. |
[7] | Wenbo CAO, Yilang LIU, Weiwei ZHANG. Accelerated convergence method for fluid dynamics solvers based on reduced⁃order model and gradient optimization [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127090-127090. |
[8] | Guotao YANG, Zhenjiang YUE, Li LIU. Rapid prediction of global hypersonic vehicle aerothermodynamics based on adaptive sampling [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127391-127391. |
[9] | Xulong ZHANG, Weimin WANG, Tianqing LI, Yulong LIN, Xinxi AI, Zhenguo WANG. Analysis and verification of trend term for tip timing signal under variable speed condition [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 426980-426980. |
[10] | Xianbang SHEN, Kaijun YI, Xuzhen JING, Zhiyuan LIU, Rui ZHU. Design of electromechanical coupled metamaterial plates for low-frequency vibration control in aircraft structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 226959-226959. |
[11] | Ziyi WANG, Weiwei ZHANG, Lei LIU, Xiaofeng YANG. Reduced order aerothermoelastic framework suitable for complex flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 126807-126807. |
[12] | Dawei HAN, Shijie ZHENG, Youli TUO, Mingyu GE, Liming SONG, Xinqiao LI, Xiangyang WEN, Shaolin XIONG. Orbit determination analysis using Crab observation data of GECAM mission [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(3): 526641-526641. |
[13] | Jianling QIAO, Zhonghua HAN, Yulin DING, Wenping SONG, Bifeng SONG. Effects of stratified atmospheric turbulence on farfield sonic boom propagation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626350-626350. |
[14] | Fanmin MENG, Nuo MA, Wenchao MA, Junhui MENG, Wenguang LI. Wet modal analysis and tests for inflatable wing with swept air-beams [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 227098-227098. |
[15] | Weihua LI, Junlong GUO, Liang DING, Haibo GAO. State of art and prospects of ground teleoperation technology for lunar rover [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 26333-026333. |
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