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Статті в журналах з теми "High-speed liquid jet"

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KATO, Takahisa, Nobushige TAMAKI, Masanori SHIMIZU, and Hiroyuki HIROYASU. "815 Atomization of High Speed Liquid Jet." Proceedings of Conference of Chugoku-Shikoku Branch 005.2 (2000): 261–62. http://dx.doi.org/10.1299/jsmecs.005.2.261.

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Shi, H. H., J. E. Field, and C. S. J. Pickles. "High Speed Liquid Impact Onto Wetted Solid Surfaces." Journal of Fluids Engineering 116, no. 2 (June 1, 1994): 345–48. http://dx.doi.org/10.1115/1.2910278.

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The mechanics of impact by a high-speed liquid jet onto a solid surface covered by a liquid layer is described. After the liquid jet contacts the liquid layer, a shock wave is generated, which moves toward the solid surface. The shock wave is followed by the liquid jet penetrating through the layer. The influence of the liquid layer on the side jetting and stress waves is studied. Damage sites on soda-lime glass, PMMA (polymethylmethacrylate) and aluminium show the role of shear failure and cracking and provide evidence for analyzing the impact pressure on the wetted solids and the spatial pre
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Arzate, A., and P. A. Tanguy. "Hydrodynamics of Liquid Jet Application in High-Speed Jet Coating." Chemical Engineering Research and Design 83, no. 2 (February 2005): 111–25. http://dx.doi.org/10.1205/cherd.04150.

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Kanemura, Takuji, Hiroo Kondo, Hirokazu Sugiura, Hiroshi Horiike, Nobuo Yamaoka, Tomohiro Furukawa, Mizuho Ida, Izuru Matsushita, and Kazuyuki Nakamura. "ICONE19-43608 DIAGNOSTICS OF HIGH-SPEED LIQUID LITHIUM JET FOR IFMIF/EVEDA LITHIUM TEST LOOP." Proceedings of the International Conference on Nuclear Engineering (ICONE) 2011.19 (2011): _ICONE1943. http://dx.doi.org/10.1299/jsmeicone.2011.19._icone1943_246.

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Hiroyuki, Abe, Yoshida Kenji, Fukuhara Yuichi, and Kataoka Isao. "1014 MEASUREMENT OF LIQUID FRACTION DISTRIBUTION OF HIGH SPEED WATER JET BY LASER SHRIELEN METHOD." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1014–1_—_1014–6_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1014-1_.

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SHIMIZU, Masanori, Masataka ARAI, and Hiroyuki HIROYASU. "Disintegrating process of a high speed liquid jet." Transactions of the Japan Society of Mechanical Engineers Series B 54, no. 504 (1988): 2236–44. http://dx.doi.org/10.1299/kikaib.54.2236.

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Shi, Hong-Hui, Kazuyoshi Takayama, and Osamu Onodera. "Experimental Study of Pulsed High-Speed Liquid Jet." JSME International Journal Series B 36, no. 4 (1993): 620–27. http://dx.doi.org/10.1299/jsmeb.36.620.

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Hilbing, J. H., and Stephen D. Heister. "NONLINEAR SIMULATION OF A HIGH-SPEED, VISCOUS LIQUID JET." Atomization and Sprays 8, no. 2 (1998): 155–78. http://dx.doi.org/10.1615/atomizspr.v8.i2.20.

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Boiko, V. M., A. Yu Nesterov, and S. V. Poplavski. "Liquid atomization in a high-speed coaxial gas jet." Thermophysics and Aeromechanics 26, no. 3 (May 2019): 385–98. http://dx.doi.org/10.1134/s0869864319030077.

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Anufriev, I. S., E. Yu Shadrin, E. P. Kopyev, O. V. Sharypov, and V. V. Leschevich. "Liquid fuel spraying by a high-speed steam jet." Thermophysics and Aeromechanics 27, no. 4 (July 2020): 627–30. http://dx.doi.org/10.1134/s0869864320040162.

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Дисертації з теми "High-speed liquid jet"

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Weiland, Christopher Jude. "Characteristics of the High Speed Gas-Liquid Interface." Diss., Virginia Tech, 2009. http://hdl.handle.net/10919/26150.

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The objective of this dissertation was to investigate physical characteristics of high speed gas-liquid interfaces for the cases of subsonic, transonic, and supersonic gas jets submerged underwater and the transient development of an underwater projectile reaching the supercavitating state. These studies are motivated by the need to understand the basic physics associated with a novel submersible missile launcher termed the Water Piercing Missile Launcher (WPML). This dissertation presents the first study of high speed round and rectangular gas jets submerged underwater utilizing a global opt
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Zakrzewski, Sam Mechanical &amp Manufacturing Engineering Faculty of Engineering UNSW. "A Numerical and Experimental Investigation of High-Speed Liquid Jets - Their Characteristics and Dynamics." Awarded by:University of New South Wales. Mechanical and Manufacturing Engineering, 2002. http://handle.unsw.edu.au/1959.4/18653.

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A comprehensive understanding of high-speed liquid jets is required for their introduction into engine and combustion applications. Their transient nature, short lifetime, unique characteristics and the inability to take many experimental readings, has inhibited this need. This study investigates the outflow of a high-speed liquid jet into quiescent atmospheric air. The key characteristics present are, a bow shock wave preceding the jet head, an enhanced mixing layer and the transient deformation of the liquid jet core. The outflow regime is studied in an experimental and numerical manner. In
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Liu, Kaiyi. "Characterization and Control of an Electrospinning Process." University of Akron / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=akron1355239985.

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Verdier, Antoine. "Experimental study of dilute spray combustion." Thesis, Normandie, 2017. http://www.theses.fr/2017NORMIR27/document.

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La combustion diphasique implique de nombreux phénomènes physiques complexes, comprenant l'atomisation, la dispersion, l'évaporation et la combustion. Bien que la simulation numérique soit un outil performant pour aborder ces différentes interactions entre les phases liquides et gazeuses, la méthode doit être validée par des études expérimentales fiables. Par conséquent, des données expérimentales précises sur la structure de la flamme et sur les propriétés de la phase liquide et gazeuse le long des étapes d'évaporation et de combustion sont nécessaires. La complexité des configurations aérona
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Wu, Jong Shinn, and 吳忠信. "Stability Analysis of A High-Speed Liquid Jet." Thesis, 1993. http://ndltd.ncl.edu.tw/handle/48099625317033426404.

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碩士<br>中原大學<br>機械工程研究所<br>81<br>The purpose of this paper is to investigate the instability of a high-speed liqud jet issued into a ambient compressible gas. Firstly, we list the conservative equations of mass and momentum with corresponding boundary conditions. The liquid is an incompressible inviscid fluid and the gas is assumed to be a compressible inviscid fluid. Here the system is subjected to axisymmetrical and asymmetrical disturbance. Secondly, we neglect the high order nonlinear ter
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Charng-Jyh, Wang, and 王長志. "ANumerical Analysis of the Growth of Unstable Waves fir High-speed Liquid Jet Atomization." Thesis, 1999. http://ndltd.ncl.edu.tw/handle/13943476180565598536.

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碩士<br>國立海洋大學<br>機械與輪機工程學系<br>87<br>The high-speed jet atomization is a topic of practical applications, such as gas-turbine combustors, diesel engines, rocket thrust chambers, and spray coatings of protective materials on surface, etc. The liquid jet atomization is related with the unstable waves on the jet surface. The unstable growth rate of the surface wave is affected by initial jet velocity, liquid viscosity, liquid surface tension, liquid/gas density ratio, the difference between liquid and gas velocity, and the initial disturbance on the jet surface. In the present study, a cylindrical
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Frommhold, Philipp Erhard. "Erzeugung und Untersuchung von schnellen Mikrotropfen für Reinigungsanwendungen." Doctoral thesis, 2015. http://hdl.handle.net/11858/00-1735-0000-0022-6022-6.

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Seit mehr als einem Jahrhundert ist ein wachsendes wissenschaftliches Interesse an Tropfen und den Vorgängen bei deren Aufprall auf die verschiedensten Substrate zu verzeichnen, wohl auch durch die Fotografien von Worthington (1908) ausgelöst. Inzwischen wurden viele Erkenntnisse durch große Fortschritte bei der experimentellen Untersuchung (z.B. mittels Hochgeschwindigkeitsaufnahmen) und durch theoretische und computergestützte Untersuchung (z.B. durch skalenfreie und numerische Modellierung) gewonnen. Trotzdem bleibt durch die Vielfältigkeit und Komplexität der Phänomene während des Tropfena
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陳天任. "Theoretical Analyses for the Atomization Model of High-speed Liquid Jets." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/80734973030606586596.

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碩士<br>國立臺灣海洋大學<br>機械與機電工程學系<br>98<br>The technology of the liquid jet atomization has been widely used in many industrial and technical applications. In various engine combustion chambers, atomized drop size, velocity distribution, and breakup length have profound influences on the combustion efficiency and emission pollution. Despite a great quantity of past experimental studies, the physical process of atomization phenomenon has not been fully understood. In the present study, based on the jet surface wave instability analysis on the interface of liquid and gas, the atomization model for t
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Zakrzewski, Sam. "A numerical and experimental investigation of high-speed liquid jets : their characteristics and dynamics /." 2002. http://www.library.unsw.edu.au/~thesis/adt-NUN/public/adt-NUN20021108.042745/index.html.

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Частини книг з теми "High-speed liquid jet"

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Iyengar, Venkat S., K. Sathiyamoorthy, J. Srinivas, P. Pratheesh Kumar, and P. Manjunath. "Measurements of Droplet Velocity Fields in Sprays from Liquid Jets Injected in High-Speed Crossflows Using PIV." In Proceedings of the National Aerospace Propulsion Conference, 93–102. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5039-3_5.

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Тези доповідей конференцій з теми "High-speed liquid jet"

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Wang, Xiao-Liang, Hong-Hui Shi, Motoyuki Itoh, and Masami Kishimoto. "Flow visualization of high-speed pulsed-liquid jet." In 24th International Congress on High-Speed Photography and Photonics, edited by Kazuyoshi Takayama, Tsutomo Saito, Harald Kleine, and Eugene V. Timofeev. SPIE, 2001. http://dx.doi.org/10.1117/12.424250.

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Gong, Chen, Minguan Yang, Yuli Wang, Longlong Yan, and Bo Gao. "Turbulence Structure on the Surface of High Speed Liquid Jet." In ASME/JSME/KSME 2015 Joint Fluids Engineering Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/ajkfluids2015-09512.

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The structures on the surface of high-speed capillary liquid jet were captured with the help of high-speed camera and microscope. A power spectral density method is used to deal with the jet images. Based on captured jet image, the variation of surface structures near the exit of the nozzle is divided into three sections: laminar section, instability section and turbulence section. There is no clearly surface structures in the laminar section. The wave-like structures come out in the instability section with a sudden and are regularly increase with a small slope along the streamwise. The degre
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Stasicki, Boleslaw, Ales Charvat, Manfred Faubel, and Bernd Abel. "Visualization of laser-induced liquid micro-jet disintegration by means of high-speed video stroboscopy." In 26th International Congress on High-Speed Photography and Photonics, edited by Dennis L. Paisley, Stuart Kleinfelder, Donald R. Snyder, and Brian J. Thompson. SPIE, 2005. http://dx.doi.org/10.1117/12.567439.

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Bianchi, Gian Marco, Fabio Minelli, Ruben Scardovelli, and Stephan Zaleski. "3D Large Scale Simulation of the High-Speed Liquid Jet Atomization." In SAE World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2007. http://dx.doi.org/10.4271/2007-01-0244.

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CHEN, T., C. SMITH, D. SCHOMMER, and A. NEJAD. "Multi-zone behavior of transverse liquid jet in high-speed flow." In 31st Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-453.

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Mckeage, James W., Kieran A. Brennan, Geehoon Park, N. Catherine Hogan, Ian W. Hunter, Bryan P. Ruddy, Poul M. F. Nielsen, and Andrew J. Taberner. "High-speed X-ray analysis of liquid delivery during jet injection." In 2017 39th Annual International Conference of the IEEE Engineering in Medicine and Biology Society (EMBC). IEEE, 2017. http://dx.doi.org/10.1109/embc.2017.8036821.

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Chakraborty, Arnab, and Srikrishna Sahu. "Liquid Atomization in a High-Speed Slinger Atomizer." In ASME 2019 Gas Turbine India Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gtindia2019-2616.

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Abstract The present research aims to investigate the liquid atomization process in a slinger atomizer test rig that houses a high-speed motor which allows high rotational speed of the slinger disc. Instead of delivering the liquid directly on the slinger disc, which is commonly reported in the literature, a stationary manifold was designed that receives the liquid from the pump and supply multiple liquid jets that impinge on the rotating slinger disc. The liquid jet breakup process was visualized using front light illumination technique. All experiments were performed using water as the worki
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Balasubramanyam, Madhanabharatam, and Chien Chen. "Finite Conductivity Evaporation Modeling of Liquid Jet in High-Speed Cross-Flow." In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-833.

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Chandh, Aravind, Shivam Patel, Oleksandr Bibik, Subodh Adhikari, David Wu, Reza Rezvani, Dustin Davis, Tim Lieuwen, and Benjamin Emerson. "High Speed OH PLIF Measurements of Combustor Effusion Films in a High Pressure, Liquid Fueled Combustor." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-59306.

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Abstract This paper presents measurements of 10 kHz OH planar laser induced fluorescence (PLIF) with an objective to study the interaction of effusion cooling with the flame and hot combustion products in the liquid fueled combustor. The combustor rig is a single sector representation a rich-burn/quick-quench/lean-burn (RQL) configuration. It consists of a swirl nozzle, dilution, and effusion jets. The rig is operated under realistic aircraft conditions, including elevated combustor inlet temperature, and elevated pressure. The PLIF laser sheet was arranged perpendicular and parallel to the li
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Bianchi, Gian Marco, Piero Pelloni, Stefano Toninel, Ruben Scardovelli, Anthony Leboissetier, and Stephan Zaleski. "A Quasi-Direct 3D Simulation of the Atomization of High-Speed Liquid Jets." In ASME 2005 Internal Combustion Engine Division Spring Technical Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/ices2005-1067.

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In this paper a quasi-direct solution of transient three-dimensional CFD calculations based on a finite volume approach has been adopted to simulate the atomization process of high velocity liquid jets issuing an injector-like nozzle. An accurate Volume-of-Fluid (VOF) method is used to reconstruct and advect the interface between the liquid and gas phases. An extended mesh which includes the injector nozzle and the upstream plenum has been considered in order to investigate accurately the effect of nozzle flow conditions on the liquid jet atomization. Cavitation modeling has not been included
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