Dynamic response of fiber–metal laminates (FMLs) subjected to low-velocity impact

Payeganeh, G.H.; Ghasemi, Faramarz Ashenai; Malekzadeh, K.

doi:10.1016/j.tws.2009.07.005

Cited by 68 publications

(47 citation statements)

References 28 publications

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“…1 (Payeganeh et al, 2010). Figure 1 Schematic view of the FML impacted by a spherical mass on its center (Payeganeh et al, 2010) …”

Section: Governing Equationsmentioning

confidence: 99%

“…2 (Payeganeh et al, 2010) shows a two-degrees of freedom springs-masses model is used to determine the impact force (Fig. 2).…”

Section: Contact Force Analysismentioning

confidence: 99%

“…Figure 2 A two-degrees of freedom springs-masses model (Payeganeh et al, 2010) which the index 1 indicates the plate and the index 2 belongs to the impactor. F is the contact force, m 1 =m p and m 2 =m i represents respectively the mass of the impactor and the FML plate, z 1 and z 2 are respectively the relative displacements of the structure and the impactor masses, K 1 = K bs is the bending-shear stiffness the plate.…”

Section: Contact Force Analysismentioning

confidence: 99%

“…They were made to combine the good properties (such as impact resistance) of the metals with the better lightweight characteristic of FRPs by Vlot (1997), Caprino et al (2004, and2007), Atas (2007) and Abdullah and Cantwell (2006). This makes them to be an alternative to aluminum in aerospace industries as presented by Payeganeh et al (2010), Asundi and Choi (1997) and Marsh (2005). Abrate (1991Abrate ( , 1994Abrate ( , and 2001) studied the impact behavior of composite materials in a widespread way.…”

Section: Introductionmentioning

confidence: 99%

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Analytical and Mathematical Modeling and Optimization of Fiber Metal Laminates (FMLs) subjected to low-velocity impact via combined response surface regression and zero-One programming

Ghasemi

Raissi

Malekzadehfard

2013

Lat. Am. j. solids struct.

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This paper presents analytical and mathematical modeling and optimization of the dynamic behavior of the fiber metal laminates (FMLs) subjected to low-velocity impact. The deflection to thickness (w/h) ratio has been identified through the governing equations of the plate that are solved using the first-order shear deformation theory as well as the Fourier series method. With the help of a two degrees-of-freedom system, consisting of springs-masses, and the Choi's linearized Hertzian contact model the interaction between the impactor and the plate is modeled. Thirty-one experiments are conducted on samples of different layer sequences and volume fractions of Al plies in the composite Structures. A reliable fitness function in the form of a strict linear mathematical function constructed. Using an ordinary least square method, response regression coefficients estimated and a zero-one programming technique proposed to optimize the FML plate behavior subjected to any technological or cost restrictions. The results indicated that FML plate behavior is highly affected by layer sequences and volume fractions of Al plies. The results also showed that, embedding Al plies at outer layers of the structure significantly results in a better response of the structure under low-velocity impact, instead of embedding them in the middle or middle and outer layers of the structure.

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“…1 (Payeganeh et al, 2010). Figure 1 Schematic view of the FML impacted by a spherical mass on its center (Payeganeh et al, 2010) …”

Section: Governing Equationsmentioning

confidence: 99%

“…2 (Payeganeh et al, 2010) shows a two-degrees of freedom springs-masses model is used to determine the impact force (Fig. 2).…”

Section: Contact Force Analysismentioning

confidence: 99%

Section: Contact Force Analysismentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

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Analytical and Mathematical Modeling and Optimization of Fiber Metal Laminates (FMLs) subjected to low-velocity impact via combined response surface regression and zero-One programming

Ghasemi

Raissi

Malekzadehfard

2013

Lat. Am. j. solids struct.

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“…Vlot [3] derived a non-linear method for the low-velocity response of fully clamped plates whereas Payeganeh [4] studied simply supported FMLs. Unlike these studies that are limited to elastic behaviour, Hoo Fatt [5] developed a model to determine the ballistic limit of GLARE although no test data was provided for the response.…”

Section: Introductionmentioning

confidence: 99%

Development of fibre-metal laminates for improved impact performance

Morinière

Alderliesten

Benedictus

2012

Eur. Phys. J. Spec. Top.

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Abstract. An analytical and experimental investigation into the low-velocity behaviour of GLARE Fibre-Metal Laminates (FMLs) has been performed. A quasi-static approach was developed to estimate the perforation energy absorbed between the constituents of GLARE. The analysis considered contact area increase during perforation and strain rate effect on material properties. Particular attention was paid to the effect of ply-angle orientation and aluminium position. Predicted maximum impact force, maximum displacement, and perforation energy related to impact velocity were within 10% of test results. Stacking composite plies oriented along the diagonal of the plate with more than 2 aluminium layers leads to a more impact resistant FML. The generic nature of the developed methodology can support the optimization of high-performance FML concepts.

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Effect of multiphase fiber system and stacking sequence on low‐velocity impact and residual tensile behavior of glass/epoxy composite laminates

2018

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This article investigates the effect of multiphase fiber system based on plain weave woven fabrics and chopped short fibers in glass/epoxy composite laminates on low‐velocity drop weight impact and quasi‐static tensile after impact (TAI) behaviors. In this regard, glass/epoxy composites with two stacking sequences (intercalated and sandwich‐like lay‐ups) were tested and compared with homogeneous standard composites fabricated with either only woven or only chopped fibers. In all the samples with multiphase fiber system, the amount of woven and chopped glass fibers were equal (4 layers and 3 layers, respectively), while stacking sequences were different. This enabled us to investigate the associated influences of fiber architecture and stacking sequence on low‐velocity drop weight impact and TAI behavior of the glass/epoxy composite laminates. All the glass/epoxy samples were impacted at four various impact energy levels, particularly 2, 4, 6, and 8 J. Results depicted that fiber architecture and stacking sequence played a vital role in low‐velocity drop weight impact and TAI behavior (i.e., damage degree, absorbed energy, peak contact force, residual deformation, residual tensile strength, displacement to ultimate failure, and failure profile) of the glass/epoxy samples. The results depicted that the sandwich‐like lay‐up configuration presented superior impact properties and damage tolerance capabilities at low impact energies (up to 4 J). On the contrary, intercalated lay‐up arrangement suited better to withstand widespread damage generated by higher impact energy levels (6 and 8 J), because they enabled a more efficient redistribution of low‐velocity impact damage in the composite. POLYM. COMPOS., 40:1450–1462, 2019. © 2018 Society of Plastics Engineers

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Dynamic response of fiber–metal laminates (FMLs) subjected to low-velocity impact

Cited by 68 publications

References 28 publications

Analytical and Mathematical Modeling and Optimization of Fiber Metal Laminates (FMLs) subjected to low-velocity impact via combined response surface regression and zero-One programming

Analytical and Mathematical Modeling and Optimization of Fiber Metal Laminates (FMLs) subjected to low-velocity impact via combined response surface regression and zero-One programming

Development of fibre-metal laminates for improved impact performance

Effect of multiphase fiber system and stacking sequence on low‐velocity impact and residual tensile behavior of glass/epoxy composite laminates

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