RELIABILITY OF UNCERTAIN LAMINATED SHELLS DUE TO BUCKLING AND SUPERSONIC FLUTTER

被引:17
|
作者
LIAW, DG
YANG, HTY
机构
[1] School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN
[2] Purdue University, West Lafayette, IN
基金
美国国家科学基金会;
关键词
D O I
10.2514/3.10793
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An objective of this paper is to study the supersonic flutter characteristics of initially compressed, laminated, thin shell structures using a 48-degree-of-freedom, doubly curved, quadrilateral, laminated, thin shell finite element developed on the basis of the Kirchhoff-Love thin shell theory and classical lamination theory. The aerodynamic pressure due to supersonic potential flow is described by the piston theory. Another objective of this paper is to study the reliability of initially compressed, laminated thin shells with structural uncertainties due to variabilities that occurred during fabrication. The two failure criteria considered are buckling and supersonic flutter. Interactive effects between the middle surface load and aerodynamic pressure for the uncertain shells are also studied. For buckling analysis, the structural uncertainties include modulus of elasticity, thickness, and fiber orientation of individual lamina, as well as geometric imperfections of the entire shell. For flutter analysis, additional uncertainties of mass densities of both the shell and the air, as well as the amplitudes of uniformly and linearly distributed middle surface loads, are considered. The stochastic element formulation is defined by including the effects of structural uncertainties and random middle surface loads. The stochastic solution procedure is developed based on the mean-centered, second-moment perturbation technique. To evaluate the validity and to demonstrate the applicability of the present formulation and solution procedure, a series of vibration, buckling, and supersonic flutter analyses of thin shells with structural uncertainties under random middle surface loads are performed. The results quantify the effects of these uncertain parameters on the reduction of the structural reliability and stability boundaries of initially compressed laminated shells. The results also provide physical insight into such design and fabrication problems with practical significance.
引用
收藏
页码:1698 / 1708
页数:11
相关论文
共 50 条
  • [41] Buckling of laminated composite shells under transverse load
    Ram, KSS
    Babu, TS
    COMPOSITE STRUCTURES, 2002, 55 (02) : 157 - 168
  • [42] Special Issue on Buckling of Composite Laminated Shells FOREWORD
    Degenhardt, Richard
    INTERNATIONAL JOURNAL OF STRUCTURAL STABILITY AND DYNAMICS, 2010, 10 (04) : VII - VIII
  • [43] ON THE ANALYSIS OF THE BUCKLING BEHAVIOR OF LAMINATED COMPOSITE PLATES AND SHELLS
    GEIER, B
    ROHWER, K
    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1989, 27 (02) : 403 - 427
  • [44] FINITE-ELEMENT SOLUTION OF THE SUPERSONIC FLUTTER OF CONICAL SHELLS
    BISMARCKNASR, MN
    COSTASAVIO, HR
    AIAA JOURNAL, 1979, 17 (10) : 1148 - 1150
  • [45] Buckling analysis of rotationally periodic sandwich laminated shells
    Department of Engineering Mechanics, School of Aerospace, Tsinghua University, Beijing 100084, China
    Hangkong Xuebao, 2006, 1 (50-54):
  • [46] Flutter of delaminated cross-ply laminated cylindrical shells
    Yazdi, Ali A.
    COMPOSITE STRUCTURES, 2012, 94 (09) : 2888 - 2894
  • [47] Modeling and computational simulation for supersonic flutter prediction of polymer/GNP/fiber laminated composite joined conical-conical shells
    Nasution, Mahyuddin K. M.
    Syah, Rahmad
    Ramdan, Dadan
    Afshari, Hassan
    Amirabadi, Hossein
    Selim, Mahmoud M.
    Khan, Afrasyab
    Rahman, Md Lutfor
    Sarjadi, Mohd Sani
    Su, Chia-Hung
    ARABIAN JOURNAL OF CHEMISTRY, 2022, 15 (01)
  • [48] Recent developments in investigation on buckling and post buckling responses of laminated composite shells
    Praveen, Paul A.
    Rajamohan, Vasudevan
    Mathew, Arun Tom
    POLYMER COMPOSITES, 2018, 39 (12) : 4231 - 4242
  • [49] Optimization of laminated composites subject to uncertain buckling loads
    Adali, S
    Lene, F
    Duvaut, G
    Chiaruttini, V
    COMPOSITE STRUCTURES, 2003, 62 (3-4) : 261 - 269
  • [50] UNCERTAIN BUCKLING AND RELIABILITY ANALYSIS OF THE PIEZOELECTRIC FUNCTIONALLY GRADED CYLINDRICAL SHELLS BASED ON THE NONPROBABILISTIC CONVEX MODEL
    Bi, R. G.
    Han, X.
    Jiang, C.
    Bai, Y. C.
    Liu, J.
    INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2014, 11 (06)