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Journal articles on the topic 'Low-velocity impact'

Author: Grafiati

Published: 4 June 2021

Last updated: 8 June 2024

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1

Dolganina, Natalia, and Sergey Sapozhnikov. "CHARACTERIZATION OF LOW VELOCITY LOCAL IMPACT OF SANDWICH PANELS." PNRPU Mechanics Bulletin 1 (December 30, 2014): 271–82. http://dx.doi.org/10.15593/perm.mech/2014.4.11.

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2

Anuar, Nurhamizah. "Cockleshell Structure under Low-Velocity Impact." International Journal of Emerging Trends in Engineering Research 8, no. 7 (July 25, 2020): 3023–27. http://dx.doi.org/10.30534/ijeter/2020/23872020.

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3

Flores-Johnson, EA, and QM Li. "Low velocity impact on polymeric foams." Journal of Cellular Plastics 47, no. 1 (November 24, 2010): 45–63. http://dx.doi.org/10.1177/0921374010384956.

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4

Yasaka, Tetsuo, Toshiya Hanada, and Hiroshi Hirayama. "LOW-VELOCITY PROJECTILE IMPACT ON SPACECRAFT." Acta Astronautica 47, no. 10 (November 2000): 763–70. http://dx.doi.org/10.1016/s0094-5765(00)00127-2.

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5

Trowbridge, D. A., J. E. Grady, and R. A. Aiello. "Low velocity impact analysis with nastran." Computers & Structures 40, no. 4 (January 1991): 977–84. http://dx.doi.org/10.1016/0045-7949(91)90328-j.

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6

Jones, Norman, and R. S. Birch. "Low-velocity impact of pressurised pipelines." International Journal of Impact Engineering 37, no. 2 (February 2010): 207–19. http://dx.doi.org/10.1016/j.ijimpeng.2009.05.006.

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7

Mahajan, P., and A. Dutta. "Adaptive computation of impact force under low velocity impact." Computers & Structures 70, no. 2 (January 1999): 229–41. http://dx.doi.org/10.1016/s0045-7949(98)00075-3.

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8

Samal, Sneha, David Reichmann, Iva Petrikova, and Bohdana Marvalova. "Low Velocity Impact on Fiber Reinforced Geocomposites." Applied Mechanics and Materials 827 (February 2016): 145–48. http://dx.doi.org/10.4028/www.scientific.net/amm.827.145.

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Low velocity impact strength of the fabric reinforced geocomposite has investigated in this article. Various fabrics such as carbon and E-glass were considered for reinforcement in geopolymer matrix. The primary two parameters such as low velocity, impact damage modes are explained on the E-glass and carbon based fabric geocomposite. The onset mode of damage to failure mode is examined through C-scan analysis. The quality of the composite is observed using c-scan with acoustic vibration mode of sensor before and after impact test. Then the effect of fabric and matrix on the impact behaviour is discussed. Residual strength of the composite is measured to determine post impact behaviour. It has been observed that resistance properties of E-glass reinforced composite is better than carbon fabric reinforced composite.

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9

Yeager, M., S. E. Boyd, J. M. Staniszewski, B. A. Patterson, D. B. Knorr, and T. A. Bogetti. "Modelling Low Velocity Impact on Structural Composites." IOP Conference Series: Materials Science and Engineering 987 (November 28, 2020): 012024. http://dx.doi.org/10.1088/1757-899x/987/1/012024.

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10

Bidi, A., Gh Liaghat, and Gh Rahimi. "Low-velocity impact on cylindrically curved bilayers." Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics 232, no. 4 (March 19, 2018): 568–76. http://dx.doi.org/10.1177/1464419318756661.

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In this study, low-velocity impact response of cylindrically curved bilayer panels is studied. A large number of parameters affect the impact dynamics and many models have been used for solution previously. These models can be classified as energy balance model, spring–mass model, and complete models in which the dynamic behavior of the structure is exactly modeled. In this study, a two degrees of freedom spring–mass model is used to evaluate contact force between the composite panel and impactor. This work uses the modified Hertz contact model which is linearized form of general Hertz contact law. First-order shear deformation theory coupled with Fourier series expansion is used to derive the governing equations of the curved bilayer panel. The effects of panel curvature, impact velocity, and mass of impactor on the panel behavior under low-velocity impact are investigated. The results show that changing the panel radius of curvature will change the impact force, impact duration, and local panel deformation. Finally, analytical solutions have been compared with numerical results.

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11

Melosh, H. J., and G. S. Collins. "Meteor Crater formed by low-velocity impact." Nature 434, no. 7030 (March 2005): 157. http://dx.doi.org/10.1038/434157a.

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12

Morinière, F. D., R. C. Alderliesten, and R. Benedictus. "Low-velocity impact energy partition in GLARE." Mechanics of Materials 66 (November 2013): 59–68. http://dx.doi.org/10.1016/j.mechmat.2013.06.007.

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13

Waters, Daniel H., Joseph Hoffman, Eva Hakansson, and Maciej Kumosa. "Low-velocity impact to transmission line conductors." International Journal of Impact Engineering 106 (August 2017): 64–72. http://dx.doi.org/10.1016/j.ijimpeng.2017.03.010.

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14

Lifshitz, J. M., F. Gov, and M. Gandelsman. "Instrumented low-velocity impact of CFRP beams." International Journal of Impact Engineering 16, no. 2 (April 1995): 201–15. http://dx.doi.org/10.1016/0734-743x(94)00048-2.

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15

Gustin, J., M. Mahinfalah, G. Nakhaie Jazar, and M. R. Aagaah. "Low-velocity impact of sandwich composite plates." Experimental Mechanics 44, no. 6 (December 2004): 574–83. http://dx.doi.org/10.1007/bf02428247.

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16

Bensadoun, F., D. Depuydt, J. Baets, I. Verpoest, and A. W. van Vuure. "Low velocity impact properties of flax composites." Composite Structures 176 (September 2017): 933–44. http://dx.doi.org/10.1016/j.compstruct.2017.05.005.

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17

Crupi, V., G. Epasto, and E. Guglielmino. "Low-velocity impact strength of sandwich materials." Journal of Sandwich Structures & Materials 13, no. 4 (October 13, 2010): 409–26. http://dx.doi.org/10.1177/1099636210385285.

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18

THIAGARAJAN, A., K. PALANIRADJA, and N. ALAGUMURTHI. "LOW VELOCITY IMPACT ANALYSIS OF NANOCOMPOSITE LAMINATES." International Journal of Nanoscience 11, no. 03 (June 2012): 1240008. http://dx.doi.org/10.1142/s0219581x1240008x.

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This paper presents the investigations made on the effect of impact response of glass fiber-reinforced epoxy nanocomposites. The laminates are prepared using 6 layers of glass woven roving mates of 610 gsm and MMT clay content varied from 0%, 1%, 3% and 5%. The prepared composite laminates were subjected to low-velocity impact with energy of 18 J. The methodology used for the impact test is based on the ASTM D3029 standard. During these impact tests, load–time histories, Peak load and absorbed energy were recorded by load cell. The incorporation of 1% and 3% nanoclay lead to higher load bearing capacity and energy absorption. Damages produced on the front and back surfaces of the samples were analyzed by visual inspection methods and scanning electron microscope.

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19

Chiu, Chin-Chen, and Yung Liou. "Low-velocity impact damage in brittle coatings." Journal of Materials Science 30, no. 4 (February 1995): 1018–24. http://dx.doi.org/10.1007/bf01178439.

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20

Park, Chan Yik, Kwan Ho Lee, In-Gul Kim, and Young Shin Lee. "OS09W0065 Low velocity impact monitoring for a composite sandwich beam using PVDF sensor signals." Abstracts of ATEM : International Conference on Advanced Technology in Experimental Mechanics : Asian Conference on Experimental Mechanics 2003.2 (2003): _OS09W0065. http://dx.doi.org/10.1299/jsmeatem.2003.2._os09w0065.

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21

NORDMARK, A. B. "EFFECTS DUE TO LOW VELOCITY IMPACT IN MECHANICAL OSCILLATORS." International Journal of Bifurcation and Chaos 02, no. 03 (September 1992): 597–605. http://dx.doi.org/10.1142/s0218127492000720.

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Phenomena caused by low velocity impacts in a class of forced impact oscillators are studied. It is shown that such impacts play an important role in the dynamics of general impacting systems. Features observed in numerical simulations of different oscillator models are associated with previous theoretical work on grazing impact. The Poincaré mapping geometry near points leading to low velocity impacts is shown, as well as bifurcations of types not found in nonimpacting systems. The consequences of not having a completely rigid constraint and the connection with the limiting case of a pure constraint are examined. In addition, low velocity impact in a Hamiltonian system is shown to have considerable effect on the break up of invariant tori.

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22

Gaidhankar, Darshan G., Mohammad Omid Naqshbandi, and Mrudula S. Kulkarni. "Impact Strength of Ferrocement Panel under Low Velocity Impact Loading." International Journal of Engineering and Advanced Technology 10, no. 5 (June 30, 2021): 285–91. http://dx.doi.org/10.35940/ijeat.e2677.0610521.

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The capability to absorb energy, often called as toughness, is of importance in actual service conditions of mesh reinforced composites, when they may be subjected to static, dynamic and fatigue loads. Toughness evaluated under impact loads is the impact strength. The toughness of materials are determined by two methods, (i) by measuring deformation under impact load, (ii) by determining energy adsorption capacity of materials under impact load. Several methods were used to investigate to determining toughness of materials. In this research work, drop weight impact test were used. The present experimental work describes testing of flat ferrocement panels with different number of layer steel mesh as well as enhancement of panels with steel fiber. The main purpose of this study is to investigate the effect of using different number of wire mesh layer on the flexural strength and impact strength and also effect of varying thickness of panels on the energy absorption of ferrocement panels. The experimental work includes preparation of ferrocement panels reinforced with welded square mesh, woven square mesh with and without hooked steel fibers The ferrocement panels of different sizes were prepared and tested for flexural strength under the two point loading as well as drop weight for impact testing. It is expected that as the mesh layers will be increased the energy absorption capacity of the panel should be increased and the also its effect should be seen for addition of hooked steel fibers.

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23

Ahmad, Mansoor, Dianshi Feng, and Wahab Ali. "Low Velocity Impact of Composite Materials Glass Fiber Laminates." European Journal of Applied Science, Engineering and Technology 2, no. 3 (May 1, 2024): 59–68. http://dx.doi.org/10.59324/ejaset.2024.2(3).06.

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Glass fiber reinforced polymer (GFRP) laminates are crucial in various sectors like aerospace, navigation, automotive, wind power infrastructures because their high strength-to-weight ratio and corrosion resistance. Their susceptibility to impact damage could cause severe structural failures such as delamination, fiber rupture, and matrix fractures which are big risk for public safety. This research focuses structural behavior and failure mechanisms of GFRP laminates under low-velocity impacts to improve industry safety, reliability and performance. Impact experiments were carried out using a Split Hopkinson Pressure Bar (SHPB) on panels configured in various fiber orientations, specifically [(0/90)s, (+45/-45)s, and (0/90/+45/-45)s]. Force-time history and impactor velocity, were captured and analyzed to assess the material's resilience and mechanical properties are main key experiments aspects. The purpose of the study to experimental and numerical approach to explore how GFRP laminates react to low-velocity impacts using a Split Hopkinson Pressure Bar (SHPB). Panels in various fiber orientations were tested with impact energies ranging from 1 J to 10 J by using advanced modeling techniques such as progressive damage mechanics, cohesive zone models, and virtual crack closure were implemented in the ABAQUS/Explicit framework to assess internal damages.

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24

Akshaj, Kumar V., P. Surya, and M. K. Pandit. "Low Velocity Impact Response of Composite/Sandwich Structures." Key Engineering Materials 725 (December 2016): 127–31. http://dx.doi.org/10.4028/www.scientific.net/kem.725.127.

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Dent resistance of structures is one of the important design parameters to consider in automotive, aerospace, packaging and transportation of fragile goods, civil engineering and marine industries. It is important to study the dynamic impact response of various combinations of skin and core materials which can provide desired fracture toughness and highest strength to weight ratio for such applications. This paper discusses the low velocity impact response of sandwich structures having unique combination of mild steel as skin material bonded to thermoplastics/PU foam as core material. HDPE, LDPE and polypropylene were the choice of thermoplastics and an optimum combination of materials for the sandwich structure was evaluated using drop-weight experimental set up. It is observed that LDPE is the best choice of core material for the sandwich structures considered.

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25

Kudinov, V. V., I. K. Krylov, V. I. Mamonov, and N. V. Korneeva. "Fracture of composite materials under low-velocity impact." Physics and Chemistry of Materials Treatment, no. 3 (2018): 66–71. http://dx.doi.org/10.30791/0015-3214-2018-3-66-71.

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26

Wang, H., and T. Vu-Khanh. "Low-Velocity Impact Damage in Laminated Composite Materials." Key Engineering Materials 141-143 (September 1997): 277–304. http://dx.doi.org/10.4028/www.scientific.net/kem.141-143.277.

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27

Zha, Xiao Xiong, and Hong Xin Wang. "The Low-Velocity Impact Response of Sandwich Panels." Advanced Materials Research 168-170 (December 2010): 1149–52. http://dx.doi.org/10.4028/www.scientific.net/amr.168-170.1149.

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The low velocity impact response of sandwich panels at different energy levels has been investigated by conducting drop-weight impact tests using an instrumented falling-weight impact tower. Impact parameters like maximum impact force and the extent of the damage were evaluated and compared for different types of sandwich panels. Finite elements simulations have been undertaken using the LS-DYNA software; the results of FE simulations have a good agreement with the experiments. It shows that, the impact force increased with thickness of face-sheets and foam core, the extent of the damage increased with the impact energy, sandwich panels with steel face sheet has a good impact resistance in comparison with sandwich panel with aluminum face sheets.

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28

Zhou, Minggang, and William P. Schonberg. "Asymmetric Low-Velocity Impact of a Finite Layer." Journal of Engineering Mechanics 127, no. 5 (May 2001): 503–11. http://dx.doi.org/10.1061/(asce)0733-9399(2001)127:5(503).

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29

Kim, Bong Hwan, Kook Chan Ahn, and Chi Woo Lee. "Low Velocity Impact Behaviors of a Laminated Glass." Smart Science 2, no. 4 (January 2014): 209–13. http://dx.doi.org/10.1080/23080477.2014.11665628.

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30

Lee, I. T., Y. Shi, A. M. Afsar, Y. Ochi, S. I. Bae, and J. I. Song. "Low Velocity Impact Behavior of Aluminum Honeycomb Structures." Advanced Composite Materials 19, no. 1 (January 2010): 19–39. http://dx.doi.org/10.1163/156855109x434810.

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31

Zhu, Shengqing, and Gin Boay Chai. "Low-velocity impact response of composite sandwich panels." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 230, no. 2 (February 9, 2015): 388–99. http://dx.doi.org/10.1177/1464420715572236.

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32

Miller, David B. "Low Velocity Impact, Vehicular Damage and Passenger Injury." CRANIO® 16, no. 4 (October 1998): 226–29. http://dx.doi.org/10.1080/08869634.1998.11746061.

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33

Singh, Hariveer, Bulon Ch Hazarika, and Sudip Dey. "Low Velocity Impact Responses of Functionally Graded Plates." Procedia Engineering 173 (2017): 264–70. http://dx.doi.org/10.1016/j.proeng.2016.12.010.

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34

Rizov, Victor Iliev. "Low velocity localized impact study of cellular foams." Materials & Design 28, no. 10 (January 2007): 2632–40. http://dx.doi.org/10.1016/j.matdes.2006.09.023.

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35

Sjoblom, Peter O., J. Timothy Hartness, and Tobey M. Cordell. "On Low-Velocity Impact Testing of Composite Materials." Journal of Composite Materials 22, no. 1 (January 1988): 30–52. http://dx.doi.org/10.1177/002199838802200103.

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36

Roh, Jin-Ho, and Ji-Hwan Kim. "Hybrid smart composite plate under low velocity impact." Composite Structures 56, no. 2 (May 2002): 175–82. http://dx.doi.org/10.1016/s0263-8223(01)00189-1.

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37

Lam, K. Y., and T. S. Sathiyamoorthy. "Low-velocity impact response for laminated stepped beam." Composite Structures 35, no. 4 (August 1996): 343–55. http://dx.doi.org/10.1016/s0263-8223(96)00009-8.

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38

Woldesenbet, Eyassu. "Low velocity impact properties of nanoparticulate syntactic foams." Materials Science and Engineering: A 496, no. 1-2 (November 2008): 217–22. http://dx.doi.org/10.1016/j.msea.2008.05.024.

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39

Zhang, Jianxun, Kang Liu, Yang Ye, and Qinghua Qin. "Low-velocity impact of rectangular multilayer sandwich plates." Thin-Walled Structures 141 (August 2019): 308–18. http://dx.doi.org/10.1016/j.tws.2019.04.033.

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40

Schubel, Patrick M., Jyi-Jiin Luo, and Isaac M. Daniel. "Low velocity impact behavior of composite sandwich panels." Composites Part A: Applied Science and Manufacturing 36, no. 10 (October 2005): 1389–96. http://dx.doi.org/10.1016/j.compositesa.2004.11.014.

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41

Caprino, G., G. Spataro, and S. Del Luongo. "Low-velocity impact behaviour of fibreglass–aluminium laminates." Composites Part A: Applied Science and Manufacturing 35, no. 5 (May 2004): 605–16. http://dx.doi.org/10.1016/j.compositesa.2003.11.003.

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42

Pashah, S., M. Massenzio, and E. Jacquelin. "Prediction of structural response for low velocity impact." International Journal of Impact Engineering 35, no. 2 (February 2008): 119–32. http://dx.doi.org/10.1016/j.ijimpeng.2006.12.006.

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43

Mannan, M. N., R. Ansari, and H. Abbas. "Failure of aluminium beams under low velocity impact." International Journal of Impact Engineering 35, no. 11 (November 2008): 1201–12. http://dx.doi.org/10.1016/j.ijimpeng.2007.08.005.

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44

Saini, Dikshant, and Behrouz Shafei. "Concrete constitutive models for low velocity impact simulations." International Journal of Impact Engineering 132 (October 2019): 103329. http://dx.doi.org/10.1016/j.ijimpeng.2019.103329.

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45

Hadidi, H., R. Q. Feng, and M. P. Sealy. "Low velocity impact of hybrid stacked steel plates." International Journal of Impact Engineering 140 (June 2020): 103556. http://dx.doi.org/10.1016/j.ijimpeng.2020.103556.

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46

Wu, C. L., and C. T. Sun. "Low velocity impact damage in composite sandwich beams." Composite Structures 34, no. 1 (January 1996): 21–27. http://dx.doi.org/10.1016/0263-8223(95)00127-1.

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47

Kakati, Sasanka, and D. Chakraborty. "Delamination in GLARE laminates under low velocity impact." Composite Structures 240 (May 2020): 112083. http://dx.doi.org/10.1016/j.compstruct.2020.112083.

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48

Heydari-Meybodi, M., H. Mohammadkhani, and M. R. Bagheri. "Oblique Low-Velocity Impact on Fiber-Metal Laminates." Applied Composite Materials 24, no. 3 (September 16, 2016): 611–23. http://dx.doi.org/10.1007/s10443-016-9530-3.

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49

Abarotin, C. A., O. J. Myers, and G. J. Pataky. "Low Velocity Impact of Bistable Laminated CFRP Composites." Journal of Dynamic Behavior of Materials 5, no. 4 (July 17, 2019): 432–43. http://dx.doi.org/10.1007/s40870-019-00209-8.

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50

Chiu, Sheng-Tsong, Yie-Yih Liou, Yuan-Chang Chang, and Ching-long Ong. "Low velocity impact behavior of prestressed composite laminates." Materials Chemistry and Physics 47, no. 2-3 (February 1997): 268–72. http://dx.doi.org/10.1016/s0254-0584(97)80063-6.

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