研究者業績

小川 隆申

オガワ タカノブ  (Takanobu Ogawa)

基本情報

所属
成蹊大学 理工学部 理工学科 教授
学位
博士(工学)(東京大学)
工学修士(東京工業大学)

J-GLOBAL ID
200901055183296938
researchmap会員ID
1000361406

外部リンク

研究キーワード

 2

経歴

 8

論文

 12
  • Yu Nishio, Takanobu Ogawa, Yuki Toda, Masataka Morimatsu, Ryohei Unno, Ayumu Inasawa
    Journal of Fluid Science and Technology 17(4) 1-15 2022年11月  査読有り
  • 井内 勝哉, 西尾 悠, 脊戸 和寿, 小川 隆申
    リメディアル教育研究 16(1) 161-167 2022年8月  査読有り
  • Tatsuma Kawachi, Takuto Sasaki, Aya Kaneko, Yu Nishio, Takanobu Ogawa
    Volume 2: Fluid Applications and Systems; Fluid Measurement and Instrumentation 2021年8月10日  
    <title>Abstract</title> The present study investigates the flow field in a rinsing process of a beverage can numerically and experimentally. The three-dimensional Navier-Stokes equations are solved with a finite volume method along with the volume of fluid (VOF) method for free surface. The beverage can set upside down is transported with a constant velocity and rinsed with a water jet ejected from a nozzle below the can. The case of a can at rest is also simulated. The result shows that the ejected water impinges on the can bottom and spreads along the side surface of the can. Then, as it flows down toward the can mouth, its front surface forms splashes. For the stationary can case, after the jet impinges on the can bottom, it almost evenly spreads over the side surface. The water flows downward and becomes branched flows by fingering. The time average of VOF is calculated to visualize the regions rinsed by water. For the case of a moving can, only the top region of the can is rinsed, and the ratio of the rinsed region drops to 29% from 69% for the stationary case. The computed water surfaces qualitatively agree with the experimental result, but the shape of the front surface, such as splashes and fingerings, cannot be resolved with the simulation.
  • Yu Nishio, Ryotaro Miyazaki, Takanobu Ogawa
    Volume 2: Fluid Applications and Systems; Fluid Measurement and Instrumentation 2021年8月10日  
    <title>Abstract</title> Micro air vehicles (MAVs) have been developed for many fields. The MAVs usually receive strong impact from a velocity change in time or space, and facilities for aerodynamic experiments of MAVs under a gusty environment have been required. The present study has developed a gust wind tunnel to generate unsteady and non-uniform flows. We developed a small wind tunnel with eight multi-fans and a shutter mechanism at the upstream of the test section. We controlled the outputs of the fans independently and obtained a linear shear layer with an error of 5 percent. The velocity gradient of the shear layer was from 5 to 8 s−1. The shutter mechanisms provided a longitudinal gust with the velocity change from 2 m/s to 10 m/s within 0.3 seconds.
  • Yu Nishio, Takanobu Ogawa, Keiji Niwa, Hirohisa Chiba
    Journal of Food Engineering 291 110237-110237 2021年2月  査読有り

MISC

 64

書籍等出版物

 2

共同研究・競争的資金等の研究課題

 11