Aerothermoelastic flutter analysis and active vibration suppression of nonlinear composite laminated panels with time-dependent boundary conditions in supersonic airflow

被引:22
作者
Chai, Yuyang [1 ]
Li, Fengming [1 ,2 ,3 ]
Song, Zhiguang [4 ]
Zhang, Chuanzeng [3 ]
机构
[1] Harbin Inst Technol, Sch Astronaut, POB 137, Harbin 150001, Heilongjiang, Peoples R China
[2] Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin, Heilongjiang, Peoples R China
[3] Univ Siegen, Dept Civil Engn, Siegen, Germany
[4] Tech Univ Darmstadt, Inst Numer Methods Mech Engn, Dynam & Vibrat Grp, Darmstadt, Germany
基金
中国国家自然科学基金;
关键词
Nonlinear composite laminated panel; time-dependent boundary conditions; aerothermoelastic analysis; macro fiber composite; aerothermal postbuckling; active flutter suppression; BEHAVIOR; PLATE; MODEL;
D O I
10.1177/1045389X17721027
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Aerothermoelastic flutter properties of nonlinear composite laminated panels in supersonic airflow are studied, and investigations on active flutter and aerothermal postbuckling suppression for the panels with time-dependent boundary conditions are also carried out using macro fiber composite actuator and sensor. The von Karman strain-displacement relation in conjunction with the supersonic piston theory is applied in structural modeling. Nonlinear dynamic equations of motion for the structural system are established using Hamilton's principle and the assumed mode method. Frequency- and time-domain methods are used to investigate the aerothermoelastic characteristics and active flutter and aerothermal postbuckling suppression of the panels. Effects of aspect ratio and ply angle on the nonlinear aerothermoelastic behaviors are studied. The displacement feedback control is used to conduct the active flutter and postbuckling suppression. The nonlinear output controller consisting of a linear quadratic regulator and a nonlinear state estimator of extended Kalman filter is also used in designing the controller. Controlled vibration responses of the structural system under the two different controllers are compared. The results show that the developed linear quadratic regulator/extended Kalman filter controller is more effective than the displacement feedback control controller in flutter and postbuckling control of the panels with time-dependent boundary conditions in supersonic airflow.
引用
收藏
页码:653 / 668
页数:16
相关论文
共 41 条
[31]   Vibration control of smart hull structure with optimally placed piezoelectric composite actuators [J].
Sohn, Jung Woo ;
Choi, Seung-Bok ;
Kim, Heung Soo .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2011, 53 (08) :647-659
[32]   Energy Harvesting Devices Using Macro-fiber Composite Materials [J].
Song, Hyun Jeong ;
Choi, Young-Tai ;
Wereley, Norman M. ;
Purekar, Ashish S. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2010, 21 (06) :647-658
[33]   Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow [J].
Song, Zhi-Guang ;
Li, Feng-Ming .
COMPOSITES PART B-ENGINEERING, 2017, 108 :334-344
[34]   Vibration analysis and optimal control of rotating pre-twisted thin-walled beams using MFC actuators and sensors [J].
Vadiraja, D. N. ;
Sahasrabudhe, A. D. .
THIN-WALLED STRUCTURES, 2009, 47 (05) :555-567
[35]   Low-cost piezocomposite actuator for structural control applications [J].
Wilkie, WK ;
Bryant, RG ;
High, JW ;
Fox, RL ;
Hellbaum, RF ;
Jalink, A ;
Little, BD ;
Mirick, PH .
SMART STRUCTURES AND MATERIAL 2000: INDUSTRIAL AND COMMERCIAL APPLICATIONS OF SMART STRUCTURES TECHNOLOGIES, 2000, 3991 :323-334
[36]  
Williams RB, 2002, AM SOC MECH ENG, V2002, P79
[37]   Study on electric-mechanical hysteretic model of Macro-Fiber Composite actuator [J].
Xue Xiaomin ;
Chen Luqi ;
Wu Xiaohong ;
Sun Qing .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2014, 25 (12) :1469-1483
[38]   Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow [J].
Zhang, L. W. ;
Song, Z. G. ;
Liew, K. M. .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2016, 300 :427-441
[39]   Modeling and simulation of macro-fiber composite layered smart structures [J].
Zhang, Shun-Qi ;
Li, Ya-Xi ;
Schmidt, Ruediger .
COMPOSITE STRUCTURES, 2015, 126 :89-100
[40]   Aeroelastic stability analysis of heated panel with aerodynamic loading on both surfaces [J].
Zhou Jian ;
Yang ZhiChun ;
Gu YingSong .
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2012, 55 (10) :2720-2726