Optimal fiber volume fraction prediction of layered composite using frequency constraints- A hybrid FEM approach

被引:14
作者
Anil, K. Lalepalli [1 ]
Panda, Subrata K. [1 ]
Sharma, Nitin [2 ]
Hirwani, Chetan K. [3 ]
Topal, Umut [4 ]
机构
[1] Natl Inst Technol Rourkela, Rourkela 769008, Odisha, India
[2] KIIT, Sch Mech Engn, Bhubaneswar 751024, Odisha, India
[3] Natl Inst Technol Patna, Deparment Mech Engn, Patna, Bihar, India
[4] Karadeniz Tech Univ, Dept Civil Engn, Fac Technol, Trabzon, Turkey
关键词
HSDT; PSO; laminated composite; optimization; fiber volume fraction; STACKING-SEQUENCE OPTIMIZATION; MAXIMUM FUNDAMENTAL-FREQUENCY; BUCKLING LOAD; DIFFERENTIAL EVOLUTION; LIGHTWEIGHT DESIGN; GENETIC ALGORITHM; LAYERWISE OPTIMIZATION; PLATES; MAXIMIZATION; VIBRATION;
D O I
10.12989/cac.2020.25.4.303
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this research, a hybrid mathematical model is derived using the higher-order polynomial kinematic model in association with soft computing technique for the prediction of best fiber volume fractions and the minimal mass of the layered composite structure. The optimal values are predicted further by taking the frequency parameter as the constraint and the projected values utilized for the computation of the eigenvalue and deflections. The optimal mass of the total layered composite and the corresponding optimal volume fractions are evaluated using the particle swarm optimization by constraining the arbitrary frequency value as mass/volume minimization functions. The degree of accuracy of the optimal model has been proven through the comparison study with published well-known research data. Further, the predicted values of volume fractions are incurred for the evaluation of the eigenvalue and the deflection data of the composite structure. To obtain the structural responses i.e. vibrational frequency and the central deflections the proposed higher-order polynomial FE model adopted. Finally, a series of numerical experimentations are carried out using the optimal fibre volume fraction for the prediction of the optimal frequencies and deflections including associated structural parameter.
引用
收藏
页码:303 / 310
页数:8
相关论文
共 44 条
[1]   OPTIMAL-DESIGN OF HYBRID LAMINATES WITH DISCRETE PLY ANGLES FOR MAXIMUM BUCKLING LOAD AND MINIMUM-COST [J].
ADALI, S ;
RICHTER, A ;
VERIJENKO, VE ;
SUMMERS, EB .
COMPOSITE STRUCTURES, 1995, 32 (1-4) :409-415
[2]  
Altenbach H., 2004, MECH COMPOSITE STRUC
[3]  
[Anonymous], 2003, CONCEPTS APPL FINITE
[4]   The Artificial Bee Colony algorithm in layer optimization for the maximum fundamental frequency of symmetrical laminated composite plates [J].
Apalak, M. Kemal ;
Karaboga, Dervis ;
Akay, Bahriye .
ENGINEERING OPTIMIZATION, 2014, 46 (03) :420-437
[5]   Layer Optimization for Maximum Fundamental Frequency of Rigid Point-Supported Laminated Composite Plates [J].
Apalak, Z. Gul ;
Apalak, M. Kemal ;
Ekici, R. ;
Yildirim, M. .
POLYMER COMPOSITES, 2011, 32 (12) :1988-2000
[6]   Optimization of laminate stacking sequence for maximum buckling load using the ant colony optimization (ACO) metaheuristic [J].
Aymerich, F. ;
Serra, M. . .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2008, 39 (02) :262-272
[7]   Stacking sequence optimization of composite plates for maximum fundamental frequency using particle swarm optimization algorithm [J].
Bargh, H. Ghashochi ;
Sadr, M. H. .
MECCANICA, 2012, 47 (03) :719-730
[8]   A NOVEL HIGHER ORDER SHEAR AND NORMAL DEFORMATION THEORY BASED ON NEUTRAL SURFACE POSITION FOR BENDING ANALYSIS OF ADVANCED COMPOSITE PLATES [J].
Bousahla, Abdelmoumen Anis ;
Houari, Mohammed Sid Ahmed ;
Tounsi, Abdelouahed ;
Bedia, El Abbas Adda .
INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2014, 11 (06)
[9]   Design Optimization of Laminated Composite Plates with Static and Dynamic Considerations in Hygrothermal Environments [J].
Cho, Hee-Keun .
INTERNATIONAL JOURNAL OF PRECISION ENGINEERING AND MANUFACTURING, 2013, 14 (08) :1387-1394
[10]  
Eberhart RC, 2001, IEEE C EVOL COMPUTAT, P81, DOI 10.1109/CEC.2001.934374