Exact solution for nonlinear thermal stability of hybrid laminated composite Timoshenko beams reinforced with SMA fibers

被引:61
作者
Asadi, H. [1 ]
Kiani, Y. [1 ]
Shakeri, M. [1 ]
Eslami, M. R. [1 ]
机构
[1] Amirkabir Univ Technol, Dept Mech Engn, Thermoelast Ctr Excellence, Tehran, Iran
关键词
Shape memory alloy; SMA Brinson model; Nonlinear thermal stability; Thermal buckling; Exact solution; BUCKLING CONTROL; FREE-VIBRATION; MEMORY; PLATES; BEHAVIOR; SHELLS;
D O I
10.1016/j.compstruct.2013.09.010
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Post-buckling behavior of Shape Memory Alloy (SMA) hybrid composite laminated beams under uniform heating is investigated in this paper. Properties of the constituents are temperature-dependent. The von-Karman type of geometrical non-linearity suitable for small strains and moderate rotations is taken into account. Displacement field through the beam obeys the kinematics of first order shear deformation theory of Timoshenko. To model the SMA fibers, the one-dimensional thermomechanical constitutive law proposed earlier by Brinson (1993) [1], is implemented. These basic assumptions are incorporated with the static version of virtual displacements to extract the nonlinear governing equations of the beam. The resulting system of nonlinear equations are uncoupled and solved analytically. Closed-form expressions are presented to trace the deflection-temperature as well as bending moment-temperature and end-shortening force-temperature in heating process. After validating the proposed approach, various parametric studies are performed to study the influence of lay-up, SMA volume fraction, SMA prestrain, boundary condition, and thickness of the layer in which SMA fibers are embedded. Fascinating results are extracted due to the recovery stress of SMA fibers. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:811 / 822
页数:12
相关论文
共 34 条
[1]  
[Anonymous], 1983, TM83320 NASA
[2]   A one-dimensional model for superelastic shape-memory alloys with different elastic properties between austenite and martensite [J].
Auricchio, F ;
Sacco, E .
INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 1997, 32 (06) :1101-1114
[4]   Stability of functionally graded shape memory alloy sandwich panels [J].
Birman, V .
SMART MATERIALS & STRUCTURES, 1997, 6 (03) :278-286
[6]  
BIRMAN V, 1995, 951210CP AIAA, P433
[7]  
Birman V., 1997, Appl. Mech. Rev, V50, P629, DOI DOI 10.1115/1.3101674
[8]   Simplifications and comparisons of shape memory alloy constitutive models [J].
Brinson, LC ;
Huang, MS .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 1996, 7 (01) :108-114
[9]  
Brinson LC., 1993, J INTEL MAT SYST STR, V4, P229, DOI DOI 10.1177/1045389X9300400213
[10]   Thermal buckling of laminated composite beams with embedded shape memory alloy actuators [J].
Choi, S ;
Lee, JJ ;
Lee, DC .
JOURNAL OF COMPOSITE MATERIALS, 2000, 34 (18) :1529-1547