The effect of cut-out parameters (shapes: square and circular; position: concentric/eccentric) on the dynamic deflection values of the curved/flat layered composite panel are verified experimentally with the higher-order finite element solutions first-time. The solutions are obtained using the linear finite element model in the framework of cubic-order displacement filed functions. The necessity of higher-order kinematic model is verified by comparing the experimental transient data by conducting the different test to show the accuracy of the finite element solution. Moreover, the theoretical finite element solutions are obtained using the own experimental elastic property data for the comparison (numerical and experimental) purpose. Finally, the critical behaviour of the proposed numerical model for the dynamic analysis of damaged composite structure is examined by solving different types of example by varying the design constraint parameter including the cut-out factors (shape, size, location and eccentricity). The inclusiveness of each parameter on the time-dependent deflections is expressed in details from the various example including the comparison.
ReddyJN.On the solutions to forced motions of rectangular composite. J Appl Mech1982; 49: 403–408.
2.
ReddyJNChandrashekharaK.Geometrically non-linear transient analysis of laminated, doubly curved shells. Int J Non Linear Mech1985; 20: 79–90.
3.
ChakravortyBDBandyopadhyayNChakravortyD.Applications of FEM on free and forced vibration of laminated shells. J Eng Mech1998; 124: 1–8.
4.
KantTAroraCPVaraiyaJH.Finite element transient analysis of composite and sandwich plates based on a refined theory and a mode superposition method. Compos Struct1992; 22: 109–120.
5.
KantTKommineniJR.Geometrically non-linear transient analysis of laminated composite and sandwich shells with a refined theory and C0 finite elements. Comput Struct1994; 52: 1243–1259.
6.
KantTKommineniJ.Geometrically non-linear analysis of symmetrically laminated composite and sandwich shells with a higher-order theory and C0 finite elements. Compos Struct1994; 27: 403–418.
7.
PradyumnaSBandyopadhyayJN.Dynamic instability behavior of laminated hypar and conoid shells using a higher-order shear deformation theory. Thin-Walled Struct2011; 49: 77–84.
8.
BiswasDRayC.Comparative study on transient response analysis of hybrid laminated composite plates with experimental verification. J Sound Vib2019; 453: 43–64.
9.
ChenJDaweDJ.Linear transient analysis of rectangular laminated plates by a finite strip-mode superposition method. Compos Struct1996; 35: 213–228.
10.
WangSChenJDaweDJ.Linear transient analysis of rectangular laminates using spline finite strips. Compos Struct1998; 41: 57–66.
11.
ChenCCKitipornchaiSLimCW, et al. Free vibration of symmetrically laminated thick-perforated plates. J Sound Vib2000; 230: 111–132.
12.
HuangXLZhengJJ.Nonlinear vibration and dynamic response of simply supported shear deformable laminated plates on elastic foundations. Eng Struct2003; 25: 1107–1119.
13.
HuangXLShenHS.Nonlinear free and forced vibration of simply supported shear deformable laminated plates with piezoelectric actuators. Int J Mech Sci2005; 47: 187–208.
14.
KhoaNDNguyenPD.Analytical investigation on nonlinear dynamic behavior and free vibration analysis of laminated nanocomposite plates. Proc Inst Mech Eng Part C:J Mechanical Engineering Science2019; 233: 6866–6878.
15.
ZhuLChattopadhyayAGoldbergRK.Multiscale analysis including strain rate dependency for transient response of composite laminated shells. J Reinf Plast Compos2006; 25: 1795–1831.
NaiduNVSSinhaPK.Nonlinear transient analysis of laminated composite shells in hygrothermal environments. Compos Struct2006; 72: 280–288.
18.
NandaNBandyopadhyayJN.Nonlinear transient response of laminated composite shells. J Eng Mech2008; 134: 983–990.
19.
NandaNBandyopadhyayJN.Geometrically nonlinear transient analysis of laminated composite shells using the finite element method. J Sound Vib2009; 325: 174–185.
20.
Moradi-DastjerdiRMomeni-KhabisiHBaghbaniR.Mesh-free dynamic analyses of FGM sandwich plates resting on a pasternak elastic foundation. Mech Adv Compos Struct2017; 4: 153–168.
21.
Moradi-DastjerdiRMomeni-KhabisiH.Vibrational behavior of sandwich plates with functionally graded wavy carbon nanotube-reinforced face sheets resting on pasternak elastic foundation. J Vib Control2018; 24: 2327–2343.
22.
Moradi-DastjerdiRPayganehGTajdariM.Resonance in functionally graded nanocomposite cylinders reinforced by wavy carbon nanotube. Polym Compos2017; 38: E542–E552.
23.
Moradi-DastjerdiRRadhiABehdinanK.Damped dynamic behavior of an advanced piezoelectric sandwich plate. Compos Struct2020; 243: 112243.
24.
AsadiHBeheshtiAR.On the nonlinear dynamic responses of FG-CNTRC beams exposed to aerothermal loads using third-order piston theory. Acta Mech2018; 229: 2413–2430.
25.
LiuCCLiFMHuangWH.Transient wave propagation and early short time transient responses of laminated composite cylindrical shells. Compos Struct2011; 93: 2587–2597.
26.
ShaoDHuFWangQ, et al. Transient response analysis of cross-ply composite laminated rectangular plates with general boundary restraints by the method of reverberation ray matrix. Compos Struct2016; 152: 168–182.
27.
ShaoDHuSWangQ, et al. A unified analysis for the transient response of composite laminated curved beam with arbitrary lamination schemes and general boundary restraints. Compos Struct2016; 154: 507–526.
28.
ShaoDHuSWangQ, et al. An enhanced reverberation-ray matrix approach for transient response analysis of composite laminated shallow shells with general boundary conditions. Compos Struct2017; 162: 133–155.
29.
MiaoFSunGChenK.Transient response analysis of balanced laminated composite beams by the method of reverberation-ray matrix. Int J Mech Sci2013; 77: 121–129.
30.
RoutMHotaSSKarmakarA.Transient response of pretwisted delaminated stiffened shell under low velocity impact. Int J Comput Methods Eng Sci Mech2018; 19: 139–155.
31.
KareemMGMajeedWI.Transient dynamic analysis of laminated shallow spherical shell under low-velocity impact. J Mater Res Technol2019; 8: 5283–5300.
32.
MantariJLOktemASGuedes SoaresC.Static and dynamic analysis of laminated composite and sandwich plates and shells by using a new higher-order shear deformation theory. Compos Struct2011; 94: 37–49.
33.
ValizadehNGhorashiSSYousefiH, et al. Transient analysis of laminated composite plates using isogeometric analysis. In: Topping BHV (ed.) Proceedings of the eighth international conference on engineering computational technology. Stirlingshire, Scotland: Civil-Comp Press. DOI: 10.4203/ccp.100.43.
34.
MalekiSTahaniMAndakhshidehA.Transient response of laminated plates with arbitrary laminations and boundary conditions under general dynamic loadings. Arch Appl Mech2012; 82: 615–630.
35.
MalekiSTahaniMAndakhshidehA.Static and transient analysis of laminated cylindrical shell panels with various boundary conditions and general lay-ups. Z Angew Math Mech2012; 92: 124–140.
36.
TornabeneFFantuzziNBacciocchiM, et al. Dynamic analysis of thick and thin elliptic shell structures made of laminated composite materials. Compos Struct2015; 133: 278–299.
37.
SahooSSPandaSKMahapatraTR.Static, free vibration and transient response of laminated composite curved shallow panel – an experimental approach. Eur J Mech – A/Solids2016; 59: 95–113.
38.
HellotyAE.Dynamic response of laminated composite shells subjected to impulsive loads. IOSR J Mech Civ Eng2017; 14: 108–123.
39.
GuoJShiDWangQ, et al. Dynamic analysis of laminated doubly-curved shells with general boundary conditions by means of a domain decomposition method. Int J Mech Sci2018; 138-139: 159–186.
40.
ChoeKKimKWangQ.Dynamic analysis of composite laminated doubly-curved revolution shell based on higher order shear deformation theory. Compos Struct2019; 225. Epub ahead of print 1 October 2019. DOI: 10.1016/j.compstruct.2019.111155.
41.
TemelBNooriAR.Transient analysis of laminated composite parabolic arches of uniform thickness. Mech Based Des Struct Mach2019; 47: 546–554.
42.
HajmohammadMHNouriAHZareiMS, et al. A new numerical approach and visco-refined zigzag theory for blast analysis of auxetic honeycomb plates integrated by multiphase nanocomposite facesheets in hygrothermal environment. Eng Comput2019; 35: 1141–1157.
43.
KantTSwaminathanK.Analytical solutions for the static analysis of laminated composite and sandwich plates based on a higher order refined theory. Compos Struct2002; 56: 329–344.
44.
KantTSwaminathanK.Analytical solutions for free vibration of laminated composite and sandwich plates based on a higher-order refined theory. Compos Struct2001; 53: 73–85.
45.
KarVRPandaSK.Free vibration responses of temperature dependent functionally graded curved panels under thermal environment. Lat Am J Solids Struct2015; 12: 2006–2024.
46.
CookRDMalkusDSPleshaME, et al. Concepts and applications of finite element analysis. 4th ed. Hoboken, NJ: John Wiley, 2002.
47.
KarVRPandaSK.Thermoelastic analysis of functionally graded doubly curved shell panels using nonlinear finite element method. Compos Struct2015; 129: 202–212.
