Stress and deformation of multiple winding angle hybrid filament-wound thick cylinder under axial loading and internal and external pressure

Xing, Jingzhong; Geng, Peng; Yang, Tiantian

doi:10.1016/j.compstruct.2015.05.036

Cited by 93 publications

(23 citation statements)

References 28 publications

(36 reference statements)

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“…Mertiny [9] have experimentally investigated the performance of multi-angle filament wound pipes subjected to bi-axial tensile stress ratios. Rafiee [10] [11] [12] have done series of investigations on industrial filament wound GRP pipes with large diameters Xia [13] [14] [15] [16] [17], Xing [18], Menshykova [19], Bakaiyan [20], Bouhafs [21] and Guedes [22][23] derived a series of exact solution based on the an-isotropic elasticity for stresses and deformations of the multi-layered filament wound composite pipes under temperature change, internal pressure, transverse and bending loading. The influence of fibre tension during filament winding process [24], filament winding manufacturing parameters [25], fibre volume fraction [26], inclined surface crack [27], defects [28] [29] and high temperature [30] [31] on the mechanical performance of FWC structure have been studied by some researchers.…”

Section: Introductionmentioning

confidence: 99%

Damage and Failure Analysis of Filament Wound Composite Structure considering Fibre Crossover and Undulation

Shen

Han

2018

Advanced Composites Letters

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The occurrence of fibre crossover and undulation(FCU) is inherent of the filament windingproc ess .However, the study on the effect of FCU on the mechanical performance and failure of filament wound composite(FWC) structure were mainly experimental research. So in this paper, a macro-meso failure analysis model for FWC considering FCU is established based on Puck, Hashin failure criterion and Linde stiffness degradation model. The influence of fibre crossove r and undulation on the stiffness failure is calculated and analyzed. The numerical results show that the strain in FCU region is higher by about 1.07-1.13 times than it in laminate region, the FCU have a certain influence on the failure strength of filament wound composite and the failure position of FWC under axial tensile load and internal pressure is mainly located FCU region and the failure position under axial compressive load is related to the winding angle.

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Section: Introductionmentioning

confidence: 99%

Damage and Failure Analysis of Filament Wound Composite Structure considering Fibre Crossover and Undulation

Shen

Han

2018

Advanced Composites Letters

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“…A large body of prior work has been completed on both the analytic and experimental analysis of composite pipes and pressure vessels [4][5][6][7][8]. Research conducted by Onder et al [4] and Xia et al [5] determined an elastic solution for the burst pressure of thick-walled composite pressure vessels with an internal pressure.…”

Section: Prior Researchmentioning

confidence: 99%

“…Research conducted by Onder et al [4] and Xia et al [5] determined an elastic solution for the burst pressure of thick-walled composite pressure vessels with an internal pressure. Xing et al [6] examined the effects of various filament-winding angles to optimize composite filamentwound pressure vessel properties and found an optimum winding angle of greater than 55 degrees and nearly 90 degrees for CFC and GFC, respectively. Hwang et al [7] investigated a novel approach for evaluating the material properties of filament-wound composite vessels with good results.…”

Section: Prior Researchmentioning

confidence: 99%

Design and Analysis of an Experimental Setup for Determining the Burst Strength and Material Properties of Hollow Cylinders

Ponshock¹

2015

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Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to ABSTRACT (maximum 200 words)A mechanical device and associated testing procedure were developed to apply internal pressure to open-ended cylinders for determination of various properties, including burst pressure, elastic modulus, and Poisson's ratio. ANSYS finite element analysis software was used to model the operation of the device with aluminum cylinders. Analytic equations for thin and thick cylinders were used to validate the computer model results. Initial mechanical testing was performed with aluminum cylinders to verify results against the finite element model. Glass and carbon fiber composite cylinders were fabricated and tested to failure with the device and the aforementioned properties were found. Finally, carbon fiber composite tensile specimens of the dog-bone shape were tested to failure to compare material properties with those found from the cylinder tests. The test device and methods developed in this research support Lawrence Livermore National Laboratory and the Defense Threat Reduction Agency in the development of the Agent Defeat Penetrator, a next-generation agent defeat weapon. SUBJECT TERMS ABSTRACTA mechanical device and associated testing procedure were developed to applyinternal pressure to open-ended cylinders for determination of various properties, including burst pressure, elastic modulus, and Poisson's ratio. ANSYS finite element analysis software was used to model the operation of the device with aluminum cylinders.Analytic equations for thin and thick cylinders were used to validate the computer model results. Initial mechanical testing was performed with aluminum cylinders to verify results against the finite element model. Glass and carbon fiber composite cylinders were fabricated and tested to failure with the device, and the aforementioned properties were found. Finally, carbon fiber composite tensile specimens of the dog-bone shape were tested to failure to compare material properties with those found from the cylinder tests.

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“…There has been extensive prior work on both the analytic and experimental analysis of composite pressure vessels and pipes [1][2][3][4][5]. Research conducted in Ref.…”

Section: Introductionmentioning

confidence: 99%

“…[1,2] determined an elastic solution for the burst pressure of thick-walled composite pressure vessels with an internal pressure. Xing et al [3] examined the effects of various filament-winding angles to optimize composite filament-wound pressure vessel properties and found an optimum winding angle for the carbon-fiber composite (CFC) and glassfiber composite (GFC) cylinders. On the other hand, Hwang et al [4] investigated a new approach for evaluating the material properties of filament-wound composite vessels.…”

Section: Introductionmentioning

confidence: 99%

Failure Loading of Metallic and Composite Cylinders Under Internal Pressure Loading

Kwon

Ponshock

Molitoris

2016

Journal of Pressure Vessel Technology

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A new mechanical device was developed to apply internal pressure loading to a cylindrical structure in order to determine its failure strength and failure mode under pressure loading. The device can be used for a uniaxial testing machine to apply internal pressure to a cylindrical structure. As a result, the developed device does not require any fluid to generate internal pressure loading. The device consists of two truncated conical shape of rams and eight pieces of the identical shape of wedges. The effectiveness of the device was assessed using both detailed finite element analyses of metallic cylinders as well as the analytical analysis. Then, a set of experimental tests were undertaken for aluminum alloy cylinders in order to evaluate experimental failure strength against the numerical and analytical results. Finally, composite cylinders made of glass-fiber or carbon-fiber woven fabrics were tested using the device, and the experimental results were compared to the predicted results using a multiscale analysis model. Those results agreed well with each other.

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Stress and deformation of multiple winding angle hybrid filament-wound thick cylinder under axial loading and internal and external pressure

Cited by 93 publications

References 28 publications

Damage and Failure Analysis of Filament Wound Composite Structure considering Fibre Crossover and Undulation

Damage and Failure Analysis of Filament Wound Composite Structure considering Fibre Crossover and Undulation

Design and Analysis of an Experimental Setup for Determining the Burst Strength and Material Properties of Hollow Cylinders

Failure Loading of Metallic and Composite Cylinders Under Internal Pressure Loading

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