Uncertain buckling characteristics of thermally loaded and internally defected variable fiber spacing composite laminates

被引:3
作者
Chandrakar, Prateek [1 ,2 ]
Sharma, Narayan [1 ]
Maiti, Dipak Kumar [1 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Kharagpur, India
[2] Indian Inst Technol, Dept Aerosp Engn, Kharagpur 721302, India
关键词
Non uniformly distributed fiber composite; variable fiber spacing composite laminated plates; thermal buckling; stochastic analysis; FINITE-ELEMENT-ANALYSIS; FIBRE/EPOXY MATRIX COMPOSITES; STRESS AMPLIFICATION FACTORS; FREE-VIBRATION; PLATES; DAMAGE; FLUTTER; STIFFNESS; BEHAVIOR; CRACKS;
D O I
10.1177/00219983241230382
中图分类号
TB33 [复合材料];
学科分类号
摘要
The present investigation underscores the efficacy of laminated plates with variable fiber spacing (VFS) in the context of internal defects. The study involves the evaluation of the variability in buckling strength when faced with multiple tiers of damage; this is achieved through the implementation of an improved first-order shear deformation theory (IFSDT) within a finite element (FE) framework. Various types of fiber distribution (DT) are being examined to evaluate the effects of damage situated at both corner and mid locations. The application of a radial basis function network (RBFN)-based surrogate model demonstrates its potential as a feasible alternative to the computationally demanding Monte-Carlo simulations (MCS) for investigating the stochastic nature of buckling; the developed surrogate model requires reduced input sampling data to quantify buckling uncertainty. This study examines the stochastic nature of different material characteristics and observed that the uncertainty in the buckling response decreases with the increased damage severity. The assessment of the probability of failure is conducted subsequently. Following this, the damage ratios are influenced by randomness, leading to the pattern that an increased damage ratio corresponds to a more pronounced deviation in buckling uncertainty.
引用
收藏
页码:723 / 754
页数:32
相关论文
共 72 条
[41]   Analytical solution approach for nonlinear vibration of shear deformable imperfect FG-GPLR porous nanocomposite cylindrical shells [J].
Salehi, Mahdi ;
Gholami, Raheb ;
Ansari, Reza .
MECHANICS BASED DESIGN OF STRUCTURES AND MACHINES, 2023, 51 (04) :2177-2199
[42]   Stochastic Finite element analysis of the free vibration of functionally graded material plates [J].
Shaker, Afeefa ;
Abdelrahman, Wael ;
Tawfik, Mohammad ;
Sadek, Edward .
COMPUTATIONAL MECHANICS, 2008, 41 (05) :707-714
[43]   Aeroelastic control of delaminated variable angle tow laminated composite plate using piezoelectric patches [J].
Sharma, Narayan ;
Swain, Prasant Kumar ;
Maiti, Dipak Kumar .
JOURNAL OF COMPOSITE MATERIALS, 2022, 56 (29) :4375-4408
[44]   Free vibration analysis of functionally graded porous plate using 3-D degenerated shell element [J].
Sharma, Narayan ;
Tiwari, Pratik ;
Maiti, Dipak Kumar ;
Maity, Damodar .
COMPOSITES PART C: OPEN ACCESS, 2021, 6
[45]   Vibration and Uncertainty Analysis of Functionally Graded Sandwich Plate Using Layerwise Theory [J].
Sharma, Narayan ;
Kumar Swain, Prasant ;
Kumar Maiti, Dipak ;
Nath Singh, Bhrigu .
AIAA JOURNAL, 2022, 60 (06) :3402-3423
[46]   Static and free vibration analyses and dynamic control of smart variable stiffness laminated composite plate with delamination [J].
Sharma, Narayan ;
Swain, Prasant Kumar ;
Maiti, Dipak Kumar ;
Singh, Bhrigu Nath .
COMPOSITE STRUCTURES, 2022, 280
[47]   Uncertainty quantification in buckling strength of variable stiffness laminated composite plate under thermal loading [J].
Sharma, Narayan ;
Nishad, Mohamed ;
Maiti, Dipak Kumar ;
Sunny, Mohammed Rabius ;
Singh, Bhrigu Nath .
COMPOSITE STRUCTURES, 2021, 275
[48]   Stochastic aeroelastic analysis of laminated composite plate with variable fiber spacing [J].
Sharma, Narayan ;
Swain, Prasant Kumar ;
Maiti, Dipak Kumar ;
Singh, Bhrigu Nath .
JOURNAL OF COMPOSITE MATERIALS, 2021, 55 (30) :4527-4547
[49]   Stochastic frequency analysis of laminated composite plate with curvilinear fiber [J].
Sharma, Narayan ;
Swain, Prasant Kumar ;
Maiti, D. K. ;
Singh, B. N. .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2022, 29 (06) :933-948
[50]   Finite Element Analysis of Thermal Buckling of Rectangular Laminated Composite Plates with Circular Cut-Out [J].
Shaterzadeh, A. R. ;
Abolghasemi, S. ;
Rezaei, R. .
JOURNAL OF THERMAL STRESSES, 2014, 37 (05) :604-623