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Dive into the research topics where Yousuke Kawashima is active.

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Featured researches published by Yousuke Kawashima.


Microgravity Science and Technology | 2007

Flow and heat transfer on cryogenic flow boiling during tube quenching under upward and downward flow

Osamu Kawanami; Teruo Nishida; Itsuro Honda; Yousuke Kawashima; Haruhiko Ohta

The gravity effects on quenching of tube by cryogenic fluids for the development of cryogenic fluid management on orbit are studied. In this paper, the effects of the tube diameter, the flow directions, and the mass velocity on the tube quenching using liquid nitrogen are investigated systematically in the terrestrial conditions. The experiments are performed by the mass velocity between 100–600 kg/m2s in downward and upward flow directions by using three difference inner diameters of the transparent heated tube (7, 10, 13.6 mm) for measuring fluid behavior observations and heat transfer measurements simultaneously. The results indicate that the difference between the minimum heat fluxes under downward and upward flow conditions increased as the mass velocity increased. These characteristics of heat transfer were caused by filamentary flow pattern that was found in only downward flow and high mass velocity conditions.


ASME 2008 6th International Conference on Nanochannels, Microchannels, and Minichannels | 2008

Flow boiling in transparent heated microtube

Osamu Kawanami; Shih Che Huang; Kazunari Kawakami; Itsuro Honda; Yousuke Kawashima; Haruhiko Ohta

In the present study, a detailed investigation of flow boiling in a transparent heated microtube was performed. The transparent heated tube was made by electroless gold plating method. The enclosed gas-liquid interface could be clearly recognized through the tube wall, and the inner wall temperature measurement and direct heating of the film were simultaneously conducted by using the tube. The experimental conditions were: tube diameter 1 mm, mass velocity 100 kg/m2 s, inlet liquid sub-cooling 20 K and heat flux up to 384 kW/m2 in the open system. Flow fluctuation was minimized by employing a twin plunger pump. Among our experimental results, we observed a high-frequency fluctuation of the inner wall temperature and a sharp peak for the heat transfer coefficient with high heat flux conditions, which have not been reported in previous experiments. This abrupt increase in the heat transfer coefficient coincided with a slight rapid axial growth of an elongated bubble found in the observation of the flow behavior. Hence, in low heat flux conditions, the fluctuations of temperature and heat transfer coefficient are strongly suppressed except for the instances when there is no bubble in the tube.Copyright


Solar Energy | 2006

Simulation on Solar Hydrogen Generation With PEM Cells and Solar Modules

Yousuke Kawashima; Osamu Kawanami; Itsurou Honda

A simulation of solar hydrogen generation with solar modules and PEM cells in consideration of the solar module temperature for one year was carried out using our measured weather data. The optimal combination of the number of PEM sheets and solar modules was determined and hydrogen conversion efficiency was estimated. Solar module temperature was predicted from the measured data of global solar radiation, ambient temperature, and wind velocity. The current-voltage (I-V) curves of a solar module in arbitrary states were calculated from the (I-V) curves in the reference states using conversion equations (JIS C8913).Copyright


Annals of the New York Academy of Sciences | 2006

A microgravity experiment of the on-orbit fluid transfer technique using swirl flow.

Osamu Kawanami; Ryoji Imai; Hisao Azuma; Haruhiko Ohta; Itsuro Honda; Yousuke Kawashima

Abstract:  The cryogenic fluid transfer technique will prove useful for flexible and low‐cost space activities by prolonging the life cycle of satellites, orbital transfer vehicles, and orbital telescopes that employ cryogenic fluids, such as reactants, coolants, and propellants. Although NASA has conducted extensive research on this technique to date, a complicated mechanism is required to control the pressure in the receiver tank and avoid a large liquid loss by vaporization. We have proposed a novel fluid transfer method by using swirl flow combined with vapor condensation facilitated by spray cooling. This technique enables gas–liquid separation in microgravity and effectively facilitates vapor condensation without any special device like a mixer. In addition, since the incoming liquid flows along the tank wall, the tank wall would be cooled effectively, thereby minimizing the liquid loss due to vaporization. In this paper, the influence of the number of inlet points, fluid velocity at the inlet, fluid type, and boiling condition on swirl flow under microgravity conditions is investigated experimentally. The results indicated that the new fluid transfer technique using the swirl flow proposed by us is effective for cryogenic fluids that generally exhibit low surface tension and good wettability. In addition, it is possible to apply this technique to the real system because the swirl flow conditions are determined by the Froude number, which is dimensionless. Thus, the fundamental technique of fluid transfer by using the swirl flow under microgravity conditions was established.


JOURNAL OF THE FLOW VISUALIZATION SOCIETY OF JAPAN | 1999

A Numerical Simulation about Collection Efficiency of Electrostatic Precipitator

Kazuhiro Murai; Itsurou Honda; Osamu Tamaki; Yousuke Kawashima

After 1980s numerical simulation approaches have been carried out in order to establish the theory for collecting particle mechanism in Electrostatic Precipitator (hereinafter, ESP). In relation to the Finite Turbulence Diffusion Model in ESP we conducted a numerical calculation to investigate fundamental flow characteristics of Electro-Hydro-Dynamics (EHD) field. In comparison of the results of laminar flow and that of turbulence flow, some significant differences between two flow patterns are there. Especially, the secondary flows by ionic wind in turbulence are smaller than in laminar and also the distribution of effective viscosity in the duct is clarified. The predicted collection efficiency by the Finite Turbulence Diffusion Model is higher than that by the Deutsch Model.


Transactions of the Japan Society of Mechanical Engineers. B | 2004

Numerical Analysis of Flow around Undulated Two-dimensional Hydrofoil

Itsuro Honda; Takanori Sanno; Kazushi Oda; Yousuke Kawashima


Microgravity Science and Technology | 2008

Experimental study of the relation between heat transfer and flow behavior in a single microtube

Shih Che Huang; Osamu Kawanami; Kazunari Kawakami; Itsuro Honda; Yousuke Kawashima; Haruhiko Ohta


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2009

Development of Non-Combustible Rocket Engine by Using Explosive Boiling of Liquid Nitrogen

Osamu Kawanami; Tomoya Suzuki; Itsuro Honda; Yousuke Kawashima


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2009

Boiling Heat Transfer Experiments by using Transparent Heated Microtube

Shih Che Huang; Osamu Kawanami; Kazunari Kawakami; Itsuro Honda; Yousuke Kawashima; Haruhiko Ohta


ASME 2009 InterPACK Conference collocated with the ASME 2009 Summer Heat Transfer Conference and the ASME 2009 3rd International Conference on Energy Sustainability | 2009

An Experimental Investigation of Flow Boiling Characteristics in a Single Transparent Heated Microtube

Osamu Kawanami; Shih Che Huang; Kazunari Kawakami; Itsuro Honda; Yousuke Kawashima; Haruhiko Ohta

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Hisao Azuma

Osaka Prefecture University

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