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Journal articles on the topic 'Impact phenomena'

Author: Grafiati

Published: 4 June 2021

Last updated: 14 February 2022

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1

Charlton, M., and G. Laricchia. "Positron impact phenomena." Journal of Physics B: Atomic, Molecular and Optical Physics 23, no. 7 (April 14, 1990): 1045–78. http://dx.doi.org/10.1088/0953-4075/23/7/004.

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2

Nicholson, Philip D. "Earth-based observations of impact phenomena." International Astronomical Union Colloquium 156 (May 1996): 81–109. http://dx.doi.org/10.1017/s0252921100115465.

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Earth-based observations at near- and mid-infrared wavelengths were obtained for at least 15 of the SL9 impacts, ranging from the spectacular G, K and L events to the barely-detected N and V impacts. Although there were a few exceptions, most of the IR lightcurves fit a common pattern of one or two relatively faint precursor flashes, followed several minutes later by the main infrared event as the explosively-ejected plume crashed down onto the jovian atmosphere. Correlations with the impact times recorded by the Galileo spacecraft and plumes imaged by the Hubble Space Telescope lead to an interpretation of the twin precursors in terms of (i) the entry of the bolide into the upper atmosphere, and (ii) the re-appearance of the rising fireball above Jupiter's limb. Positive correlations are observed between the peak IR flux observed during the splashback phase and both pre-impact size estimates for the individual SL9 fragments and the scale of the resulting ejecta deposits. None of the fragments observed to have moved off the main train of the comet by May 1994 produced a significant impact signature. Earth-based fireball temperature estimates are on the order of 750 K, 30-60 sec after impact. For the larger impacts, the unexpectedly protracted fireball emission at 2.3 μm remains unexplained. A wide range of temperatures has been inferred for the splashback phase, where shocks are expected to have heated the re-entering plume material at least briefly to several thousand K, and further modelling is required to reconcile these data.

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3

Beuhler, R., and L. Friedman. "Larger cluster ion impact phenomena." Chemical Reviews 86, no. 3 (June 1986): 521–37. http://dx.doi.org/10.1021/cr00073a003.

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4

McBride, J. W., and S. M. Sharkh. "Electrical contact phenomena during impact." IEEE Transactions on Components, Hybrids, and Manufacturing Technology 15, no. 2 (April 1992): 184–92. http://dx.doi.org/10.1109/33.142893.

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5

Langford, M. L. "Physics of Ion Impact Phenomena." International Journal of Mass Spectrometry and Ion Processes 123, no. 2 (February 1993): 167. http://dx.doi.org/10.1016/0168-1176(93)87010-p.

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6

Holsapple, Keith A. "The scaling of impact phenomena." International Journal of Impact Engineering 5, no. 1-4 (January 1987): 343–55. http://dx.doi.org/10.1016/0734-743x(87)90051-0.

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7

YAMAMURA, Yasunori. "Computer Simulations of Cluster Impact Phenomena." SHINKU 35, no. 8 (1992): 699–707. http://dx.doi.org/10.3131/jvsj.35.699.

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8

Liu, Jie, Henry Vu, Sam S. Yoon, Richard A. Jepsen, and Guillermo Aguilar. "SPLASHING PHENOMENA DURING LIQUID DROPLET IMPACT." Atomization and Sprays 20, no. 4 (2010): 297–310. http://dx.doi.org/10.1615/atomizspr.v20.i4.30.

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9

Holian, Brad Lee. "Hypervelocity-impact phenomena via molecular dynamics." Physical Review A 36, no. 8 (October 1, 1987): 3943–46. http://dx.doi.org/10.1103/physreva.36.3943.

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10

Wingate, C. A., R. F. Stellingwerf, R. F. Davidson, and M. W. Burkett. "Models of high velocity impact phenomena." International Journal of Impact Engineering 14, no. 1-4 (January 1993): 819–30. http://dx.doi.org/10.1016/0734-743x(93)90075-i.

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11

Schiehlen, Werner, Robert Seifried, and Peter Eberhard. "Elastoplastic phenomena in multibody impact dynamics." Computer Methods in Applied Mechanics and Engineering 195, no. 50-51 (October 2006): 6874–90. http://dx.doi.org/10.1016/j.cma.2005.08.011.

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12

Watson, Erkai, and Martin O. Steinhauser. "Simulating Hypervelocity Impact Phenomena with Discrete Elements." Procedia Engineering 204 (2017): 75–82. http://dx.doi.org/10.1016/j.proeng.2017.09.728.

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13

Berngardt, O. I., A. A. Dobrynina, G. A. Zherebtsov, A. V. Mikhalev, N. P. Perevalova, K. G. Ratovskii, R. A. Rakhmatulin, V. A. San’kov, and A. G. Sorokin. "Geophysical phenomena accompanying the Chelyabinsk meteoroid impact." Doklady Earth Sciences 452, no. 1 (September 2013): 945–47. http://dx.doi.org/10.1134/s1028334x13090080.

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14

Canali, C., A. Paccagnella, P. Pisoni, C. Tedesco, P. Telaroli, and E. Zanoni. "Impact ionization phenomena in AlGaAs/GaAs HEMTs." IEEE Transactions on Electron Devices 38, no. 11 (1991): 2571–73. http://dx.doi.org/10.1109/16.97428.

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15

Yoshida, H., S. Kano, Y. Hasegawa, T. Shimamon, and M. Yoshida. "Particle impact phenomena of silicon nitride ceramic." Philosophical Magazine A 74, no. 5 (November 1996): 1287–97. http://dx.doi.org/10.1080/01418619608239728.

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16

Nishida, Masahiro, Fumiya Kodama, Koichi Hayashi, Yasuhiro Akahoshi, Kazuyuki Hokamoto, and Yoshihito Kawamura. "Hypervelocity impact phenomena of LPSO-magnesium alloys." EPJ Web of Conferences 183 (2018): 02033. http://dx.doi.org/10.1051/epjconf/201818302033.

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Hypervelocity impact phenomena of long period stacking ordered type magnesium alloys (LPSO-Mg) plates were examined at the impact velocities of 4 km/s and 6 km/s. Ejecta veil and external bubble of debris of LPSO-Mg were darker than those of aluminum alloy A6061-T6. The size of external bubble of debris of LPSO-Mg was slightly smaller than that of A6061-T6. The velocity reduction of LPSOMg was slightly larger than that of A6061-T6. However, the scatter area of projectile and targets were not determined by electron probe micro-analyzer.

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17

Slătineanu, L., E. Mikhaylov, M. Coteaţă, and A. Mikhaylov. "Impact phenomena within the plasma vacuum deposition." International Journal of Material Forming 2, S1 (August 2009): 653–56. http://dx.doi.org/10.1007/s12289-009-0603-9.

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18

Omana, Martin, Daniele Rossi, TusharaSandeep Edara, and Cecilia Metra. "Impact of Aging Phenomena on Latches’ Robustness." IEEE Transactions on Nanotechnology 15, no. 2 (March 2016): 129–36. http://dx.doi.org/10.1109/tnano.2015.2494612.

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19

Marks, N. A., D. R. McKenzie, and B. A. Pailthorpe. "Molecular dynamics study of ion impact phenomena." Journal of Physics: Condensed Matter 6, no. 38 (September 19, 1994): 7833–46. http://dx.doi.org/10.1088/0953-8984/6/38/020.

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20

Gee, David J., William G. Reinecke, and Scott J. Levinson. "Blast phenomena associated with high-speed impact." International Journal of Impact Engineering 34, no. 2 (February 2007): 178–88. http://dx.doi.org/10.1016/j.ijimpeng.2005.09.002.

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21

De Carlo, A., P. Lugli, P. Pavan, E. Zanoni, and R. Malik. "Impact ionization phenomena in AlGaAs/GaAs HBTs." Microelectronic Engineering 19, no. 1-4 (September 1992): 135–38. http://dx.doi.org/10.1016/0167-9317(92)90408-j.

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22

Sudo, Seiichi, Tetsuya Yano, Yosuke Ishida, and Yoshinobu Hamada. "OS8-1-3 Interfacial Phenomena of Droplet Impact on an Air-Liquid Interface." Abstracts of ATEM : International Conference on Advanced Technology in Experimental Mechanics : Asian Conference on Experimental Mechanics 2007.6 (2007): _OS8–1–3–1—_OS8–1–3–6. http://dx.doi.org/10.1299/jsmeatem.2007.6._os8-1-3-1.

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23

Nishikawa, Chihiro, Koichi Mizutani, Tian Feng Zhou, Ji Wang Yan, and Tunemoto Kuriyagawa. "Investigation of Particle Impact Phenomena in Powder Jet Deposition Process." Key Engineering Materials 523-524 (November 2012): 184–89. http://dx.doi.org/10.4028/www.scientific.net/kem.523-524.184.

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Powder jet deposition (PJD) method is one of the blasting methods to generate surface coatings. The optimization of PJD conditions has been reported in our previous research. However, the deposition mechanism in PJD is still under investigation. Impact phenomena between an alumina particle with the mean particle size of 2 μm and a glass substrate has been successfully simulated by smoothed particle hydrodynamics (SPH) method. From the simulation result, we have deduced that a cubic particle is fractured by an impact, and it is adhered on to the substrate. It has been also deduced that substrate is removed by a spherical particle impact. Furthermore, PJD experiments of alumina particles blasted onto a glass substrate were also conducted. The particle size distribution of rectangular particles before and after impact was measured. It was found that the particle sizes after impact averagely became smaller than those before impact. The substrate was partly removed when spherical particles impact. From the results of the simulation and the experiment, we believe that the rectangular particles are fractured due to the impacts at the moment blasting onto the substrate, and then, firmly deposited on the substrate.

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24

Schonberg, William P., and Roy A. Taylor. "Penetration and ricochet phenomena in oblique hypervelocity impact." AIAA Journal 27, no. 5 (May 1989): 639–46. http://dx.doi.org/10.2514/3.10155.

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25

Peterka, Frantis̆ek. "Bifurcations and transition phenomena in an impact oscillator." Chaos, Solitons & Fractals 7, no. 10 (October 1996): 1635–47. http://dx.doi.org/10.1016/s0960-0779(96)00028-8.

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26

Jones, Norman. "Several phenomena in structural impact and structural crashworthiness." European Journal of Mechanics - A/Solids 22, no. 5 (September 2003): 693–707. http://dx.doi.org/10.1016/s0997-7538(03)00077-9.

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27

Knutson, Thomas R., and Syukuro Manabe. "Impact of increased CO2on simulated ENSO-like phenomena." Geophysical Research Letters 21, no. 21 (October 15, 1994): 2295–98. http://dx.doi.org/10.1029/94gl02152.

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28

Schonberg, William P. "Hypervelocity Impact Penetration Phenomena in Aluminum Space Structures." Journal of Aerospace Engineering 3, no. 3 (July 1990): 173–85. http://dx.doi.org/10.1061/(asce)0893-1321(1990)3:3(173).

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29

TANAKA, Katsumi. "927 Numerical study of high velocity impact phenomena." Proceedings of The Computational Mechanics Conference 2005.18 (2005): 769–70. http://dx.doi.org/10.1299/jsmecmd.2005.18.769.

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30

Watson, Erkai, and Martin Steinhauser. "Discrete Particle Method for Simulating Hypervelocity Impact Phenomena." Materials 10, no. 4 (April 2, 2017): 379. http://dx.doi.org/10.3390/ma10040379.

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31

Fiol, J., and R. O. Barrachina. "Continuum-orientation phenomena in ionization by positron impact." Journal of Physics B: Atomic, Molecular and Optical Physics 44, no. 7 (March 23, 2011): 075205. http://dx.doi.org/10.1088/0953-4075/44/7/075205.

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32

Hatesuer, Florian, Tillmann Groth, Mark Reichwage, Dieter Mewes, and Andrea Luke. "Impact of sorption phenomena on multiphase conveying processes." Heat and Mass Transfer 47, no. 8 (July 12, 2011): 921–31. http://dx.doi.org/10.1007/s00231-011-0837-1.

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33

Lambrakos, S. G., and N. E. Tran. "Inverse Analysis of Cavitation Impact Phenomena on Structures." Journal of Materials Engineering and Performance 17, no. 2 (July 11, 2007): 202–9. http://dx.doi.org/10.1007/s11665-007-9136-x.

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34

Silling, Stewart A., Michael L. Parks, James R. Kamm, Olaf Weckner, and Mostafa Rassaian. "Modeling shockwaves and impact phenomena with Eulerian peridynamics." International Journal of Impact Engineering 107 (September 2017): 47–57. http://dx.doi.org/10.1016/j.ijimpeng.2017.04.022.

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35

Klinkov, Sergei Vladimirovich, Vladimir Fedorovich Kosarev, and Martin Rein. "Cold spray deposition: Significance of particle impact phenomena." Aerospace Science and Technology 9, no. 7 (October 2005): 582–91. http://dx.doi.org/10.1016/j.ast.2005.03.005.

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36

García-Heras, Javier, Manuel Soler, Daniel González-Arribas, Kurt Eschbacher, Carl-Herbert Rokitansky, Daniel Sacher, Ulrike Gelhardt, et al. "Robust flight planning impact assessment considering convective phenomena." Transportation Research Part C: Emerging Technologies 123 (February 2021): 102968. http://dx.doi.org/10.1016/j.trc.2021.102968.

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37

PRAYONGPUN, Nuttapol, and Kosai RAOOF. "Impact of Depolarization Phenomena on Polarized MIMO Channel Performances." International Journal of Communications, Network and System Sciences 01, no. 02 (2008): 124–29. http://dx.doi.org/10.4236/ijcns.2008.12016.

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38

Jiang Ze-Hui, Li Bin, Zhao Hai-Fa, Wang Yun-Ying, and Dai Zhi-Bin. "Phenomena of impact bifurcations in vertically vibrated granular beds." Acta Physica Sinica 54, no. 3 (2005): 1273. http://dx.doi.org/10.7498/aps.54.1273.

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39

WATANABE, Keiko. "Phenomena Induced by High-Speed Impact to Particulate Materials." Journal of the Society of Materials Science, Japan 66, no. 4 (2017): 288–91. http://dx.doi.org/10.2472/jsms.66.288.

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40

Schonberg, William P., and Ahmed R. Ebrahim. "Modelling oblique hypervelocity impact phenomena using elementary shock physics." International Journal of Impact Engineering 23, no. 1 (December 1999): 823–34. http://dx.doi.org/10.1016/s0734-743x(99)00127-x.

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41

Lee, June-Yule. "The corresponding phenomena of mechanical and electronic impact oscillator." Journal of Sound and Vibration 311, no. 1-2 (March 2008): 579–87. http://dx.doi.org/10.1016/j.jsv.2007.08.034.

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42

Fojtlín, Miloš, Jan Pokorný, Jan Fišer, Róbert Toma, and Ján Tuhovčák. "Impact of measurable physical phenomena on contact thermal comfort." EPJ Web of Conferences 143 (2017): 02026. http://dx.doi.org/10.1051/epjconf/201714302026.

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43

Moreaux, Guilhem, and Georges Balmino. "Impact of some land hydrological phenomena on GOCE mission." Geophysical Research Letters 29, no. 8 (April 2002): 47–1. http://dx.doi.org/10.1029/2001gl013568.

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44

Cudnik, Brian M., David W. Palmer, David M. Palmer, Anthony Cook, Roger Venable, and Peter S. Gural. "The Observation and Characterization of Lunar Meteoroid Impact Phenomena." Earth, Moon, and Planets 93, no. 2 (October 2003): 97–106. http://dx.doi.org/10.1023/b:moon.0000034498.32831.3c.

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45

Zukas, J. A., and S. B. Segletes. "Numerical modeling of hypervelocity impact phenomena with desktop computers." Advances in Engineering Software 14, no. 1 (January 1992): 77–84. http://dx.doi.org/10.1016/0965-9978(92)90086-u.

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46

Hauser, John R. "Phenomena, theory, application, data, and methods all have impact." Journal of the Academy of Marketing Science 45, no. 1 (September 19, 2016): 7–9. http://dx.doi.org/10.1007/s11747-016-0498-1.

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47

Aleshin, Alexander S. "The antiresonance phenomena in seismic microzonation." Earthquake Engineering. Construction Safety, no. 3 (June 25, 2021): 8–18. http://dx.doi.org/10.37153/2618-9283-2021-3-8-18.

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The interference of incident and reflected seismic waves in the ground massif near the day surface is the cause of resonant effects. In the practice of seismic microzonation (SMZ), a resonant increase in the total seismic intensity is of particular importance. At the same time, the presence of inverse layers in the ground layers interference leads to a decrease in the intensity of the total seismic impact, what is naturally named antiresonance. The article considers the conditions for the occurrence of antiresonance and evaluates the limits of its effectiveness. The natural and man-made causes of antiresonance and the possibility of using it to reduce the intensity of seismic impacts are particularly noted.

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48

Akhondizadeh, Mehdi, Majid Fooladi Mahani, Masoud Rezaeizadeh, and Hoseyn S. Mansouri. "Theoretical and experimental modeling of impact wear." Industrial Lubrication and Tribology 70, no. 3 (April 9, 2018): 490–98. http://dx.doi.org/10.1108/ilt-06-2017-0159.

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Purpose Oblique impacts which occur in many situations in mineral industries leads to material removal and fail of mechanical parts. Studies will be helpful in optimal design to have minimum machine malfunctions. Design/methodology/approach In the present work, the Hertz-Di Maio Di Renzo nonlinear model of contact is used to simulate the impact phenomenon as a micro-sliding process. The modified Archard equation is used to evaluate wear over the impact. The wear coefficient is evaluated by a pin-disk machine. An impact-wear tester is used to validate the model results. Findings The measurements indicate an increase in surface hardness because of the several impacts. It is considered in the wear predictive model. Originality/value The model predictions compared with the experimental data, obtained from the impact-wear tester, show that the model well predicts the impact wear and can be used as a predictive tool to study the practical design problems and to explain some phenomena associated with the percussive impact.

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49

Roberts, Alan D. "RUBBER CONTACT PHENOMENA." Rubber Chemistry and Technology 87, no. 3 (September 1, 2014): 383–416. http://dx.doi.org/10.5254/rct.14.85982.

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ABSTRACT Research on rubber wiper blades led to the establishment of the now widely used Johnson, Kendall, Roberts (JKR) equilibrium equation that determines the strength of adhesion between surfaces. The equation was adapted to allow for the viscoelasticity of rubber, leading to explanations of how adhesion can impact on tack; rebound resilience; and rolling, static, and sliding friction. The adhesion of rubber to ice was found to depend on salt concentration in the ice, thus providing insight into winter tire performance. The development of optical techniques has greatly aided studies, particularly for measuring the thickness of thin liquid films sandwiched between rubber surfaces. Measurements on water films squeezed between rubber and glass revealed the action of repulsive surface forces that can reduce adhesion and friction. The efficacy of water lubrication depends upon whether surfactants are present and upon the acidity or alkalinity of the water. Improved understanding of adhesion and friction mechanisms offers design guidance for a range of rubber articles.

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50

Heru Utomo, Beate D., B. J. van der Meer, L. J. Ernst, and D. J. Rixen. "High Speed Fracture Phenomena in Dyneema Composite." Key Engineering Materials 353-358 (September 2007): 120–25. http://dx.doi.org/10.4028/www.scientific.net/kem.353-358.120.

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Dyneema composite is used in lightweight armour applications, because of its high specific material properties such as strength and stiffness. In armour applications, Dyneema composite is used to protect people or vehicles from projectile impact. In order to be able to guarantee a certain protection level, an accurate prediction of fracture phenomena that are caused by projectile impact is required. Currently, fracture phenomena such as delamination and fibre fracture are not accurately described. This is because a good understanding of fracture phenomena in Dyneema composite lacks. Therefore, both Dyneema fibre and Dyneema composite are analysed by different (impact) experiments to gain more insight in both the fracture phenomena as well as in the material properties. Parallel to these experiments, a start is made with the development of a new material model in ABAQUS\Explicit using cohesive zone techniques that is able to predict the fracture phenomena due to projectile impact.

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