Relevant bibliographies by topics / Indenter nose shape

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  1. Journal articles
  2. Dissertations / Theses
  3. Conference papers

Academic literature on the topic 'Indenter nose shape'

Author: Grafiati
Published: 3 June 2025
Last updated: 31 July 2025

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Journal articles on the topic "Indenter nose shape"

1

Uddin, Mohammad, Graham Stevens, and Daniel Williams. "Effect of Indenter Nose Shape and Layer Configuration on the Quasi-Static Perforation Behaviour of Metal–Plastic Laminates." Materials 15, no. 17 (2022): 5879. http://dx.doi.org/10.3390/ma15175879.

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This study investigated the perforation resistance behaviour of metal–plastic laminates (MPLs) when they are indented by different nose shapes. Aluminium (Al) and HDPE (high-density polyethylene) layers were bonded with a suitable adhesive in an alternative manner to prepare bilayer and trilayer MPL configurations. Quasi-static perforation experiments were performed with hemispherical, conical and blunt indenters. The effects of nose shape, layer configuration and adhesive on the force–deformation profile, perforation resistance capacity and failure mechanisms were evaluated. The results indic
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2

Sadeghi, Mohammad, and Mohammad Hossein Pol. "Investigation of behaviors of glass/epoxy laminate composites reinforced with carbon nanotubes under quasi-static punch shear loading." Journal of Sandwich Structures & Materials 21, no. 4 (2017): 1535–56. http://dx.doi.org/10.1177/1099636217719223.

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In this paper, in addition to investigation of the effects of adding of nanotubes on the tensile properties of epoxy matrix and glass/epoxy laminate composite, the effects of adding of nanotubes and the effect of indenter shape on quasi-static punch shear properties of glass/epoxy laminate are experimentally studied. Laminate nanocomposites have 12 layers of plain weave glass fibers which are made by hand lay-up method. Resin is composed of a two-component epoxy; Epon 828 as the base and Epikure F-205 as the curing agent. Multi-walled carbon nanotubes modified by hydroxid (–COOH) are used with
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3

Ahmadi, H., M. Ekrami, H. Sabouri, and M. Bayat. "Experimental and numerical investigation on the effect of projectile nose shape in low-velocity impact loading on fiber metal laminate panels." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 10 (2018): 3665–79. http://dx.doi.org/10.1177/0954410018804384.

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In this paper, low-velocity impact responses of 2/1 GLARE 3 (a commercial type of fiber metal laminate) specimens were studied experimentally and numerically. The effects of indenter's nose shape (flat, conical, and hemispherical) on energy absorption and failure mechanisms were thoroughly investigated. Drop weight testing machine with different impact energies was used for experimental tests and numerical simulation was also carried out. Failure mechanisms, such as delamination, debonding, aluminum sheet rupture, and composite laminate fracture, were discussed by sectioning the tested specime
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4

SampathKumar, Deepak, Thirumalaikumarasamy Duraisamy, Thirumal Pattabi, and AshokKumar Mohankumar. "Static puncture resistance characteristics with various indenter nose shape geometry perforation of shear thickening fluid impregnated polypropylene fabric for soft armour application." Polymers and Polymer Composites 30 (January 2022): 096739112110633. http://dx.doi.org/10.1177/09673911211063303.

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At present, puncture resistance and rheological performance of shear thickening fluid (STF) is an essential design requirement for a soft armour material (target sample). The target sample is prepared with a dip and dry process of STF impregnated woven polypropylene (PP) fabric. These samples were tested and compared with neat PP fabric. The penetration depth of target samples is highly sensitive to the coefficient of friction between the indenter’s nose shape geometry and the target sample. The STF is prepared by mechanical dispersion of synthesized microsphere silica microparticles at a volu
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5

Taghizadeh, Seyed Ahmad, Gholamhossein Liaghat, Abbas Niknejad, and Ehsan Pedram. "Experimental study on quasi-static penetration process of cylindrical indenters with different nose shapes into the hybrid composite panels." Journal of Composite Materials 53, no. 1 (2018): 107–23. http://dx.doi.org/10.1177/0021998318780490.

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The main aim of the present research is to investigate the quasi-static penetration process of cylindrical indenters with different nose shapes into multilayered composite panels made of Dyneema and Glass woven fibers, and aluminum face sheets. For better understanding of the perforation mechanism of the composite panels, effects of indenter geometry, stacking sequences, and boundary conditions are studied and their effects on energy absorption, specific absorbed energy, maximum deformation, peak load, and failure modes are evaluated and discussed. Samples with different layering configuration
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6

Mohagheghian, I., W. J. Stronge, and G. J. McShane. "Predicting indenter nose shape sensitivity for quasi-static perforation of thin metallic plates." European Journal of Mechanics - A/Solids 61 (January 2017): 134–50. http://dx.doi.org/10.1016/j.euromechsol.2016.09.004.

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7

Husain, Afsar, Sanan Husain Khan, Abdel Hamid I. Mourad, and Raisuddin Ansari. "Ballistic Performance of Polycarbonate Plate Subjected to Truncated Cone Projectile." Diffusion Foundations and Materials Applications 36 (November 6, 2024): 67–73. http://dx.doi.org/10.4028/p-ud2b0i.

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In the present study, a quasi-static compression test and impact test are carried out on a Polycarbonate plate with thickness of 2.66 mm and an effective diameter of 205 mm. The impact test is carried out on a pneumatic gun using a hardened truncated cone projectile of mass 25.8 g at different velocities. On the other hand, a servo mechanical universal testing machine with a 50 kN capacity is used to carry out the quasi-static compression test at a speed of 2 mm/min adopting an indenter of truncated nose shape. The Dynamic Enhancement Factor, or DEF, is computed as the ratio of quasi-static pe
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8

Guo, Zherui, James Zheng, and Weinong Chen. "Reverse ballistics penetration of Kevlar® fabric with different indenters at different loading rates." Textile Research Journal 87, no. 10 (2016): 1165–76. http://dx.doi.org/10.1177/0040517516648513.

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In this study, the mechanical load on a bullet-shaped indenter when impacted by a single-ply Kevlar fabric was experimentally investigated using a reverse ballistics method at both quasi-static and dynamic rates. Different indenter geometries, namely the 9-mm Luger, .223 Remington, and .308 Winchester bullet geometries, were used. The penetration load of the stationary indenter was measured using a force transducer located behind the indenter, and the penetration load was then plotted against the impact velocity of the fabric sample. Different mechanisms of penetration were observed at differe
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9

Dixit, A., R. K. Misra, and H. S. Mali. "Finite element analysis of quasi-static indentation of woven fabric textile composites using different nose shape indenters." Materialwissenschaft und Werkstofftechnik 46, no. 10 (2015): 1014–28. http://dx.doi.org/10.1002/mawe.201500405.

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10

Menčík, J., and M. V. Swain. "Errors associated with depth-sensing microindentation tests." Journal of Materials Research 10, no. 6 (1995): 1491–501. http://dx.doi.org/10.1557/jmr.1995.1491.

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In the determination of mechanical properties by ultra-microindentation, various errors can appear. This paper analyzes various sources of errors in estimation of elastic modulus and hardness. These errors arise from uncertainties of the indenter geometry and properties, as well as measuring instrument limitations and errors, such as the minimum detectable load, compliance, and noise of the system. Other sources of errors are thermal drift, shape of the impression, and scatter of properties of the tested material. Characteristic features and the magnitude of individual kinds of errors are disc
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Dissertations / Theses on the topic "Indenter nose shape"

1

(6504827), Boon Him Lim. "Critical Velocity of High-Performance Yarn Transversely Impacted by Different Indenters." Thesis, 2019.

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Critical velocity is defined as projectile striking velocity that causes instantaneous rupture of the specimen under transverse impact. The main goal of this dissertation was to determine the critical velocities of a Twaron<sup>®</sup> 2040 warp yarn impacted by different round indenters. Special attention was placed to develop models to predict the critical velocities when transversely impacted by the indenters. An MTS 810 load frame was utilized to perform quasi-static transverse and uniaxial tension experiments to examine the stress concentration and the constitutive mechanical properties o
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Conference papers on the topic "Indenter nose shape"

1

HOLDEN, M. "Studies of flows over indented nose shapes. I - Steady flows." In 24th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-384.

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