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Transactions of the Japan Society of Mechanical Engineers. B | 1989

Non-linear calculation of separated flow in centrifugal impellers and its application to filing problems.

Ryoji Imai; Yoshinobu Tsujimoto; A. J. Acosta

Separated flows in a centrifugal impeller are analyzed by using a singularity method on the assumption that the absolute flow is two-dimensional, steady, imcompressible, inviscid, and irrotational. By using an iterative method, the boundary conditions on the surface of separated region is applied exactly on the surface; a non-linear theory. From the angular momentum relations, it is shown that the most reasonable flow is obtained in the case when the separated region terminates with a cusped form. The velocity field and the pressure distributions are given for various flow rated and assumed separation points. The decrease in head is larger for upstream separation. Over/under filing effects are discussed by applying the present method on the assumption that the flow is separated at the trailing corners of thick vanes.


Transactions of the Japan Society of Mechanical Engineers. B | 1988

A free streamline analysis of separated flow in a centrifugal impeller.

Yoshinobu Tsujimoto; J. Allan Acosta; Ryoji Imai

The flow in a logarithmic impeller with trailing edge separation is analysed by using a conformal mapping method. The problem is linearised by assuming that the thickness of the separated region is small. The flow can be determined by specifying the location of the separation point, and by the application of the condition that there should be no singularity at the closure point. The latter condition results in the location of the closure point shortly downstream of the trailing edge. It is shown that the head is significantly reduced by the separation. Discussions are made about the angular momentum conservation relations for a few models and it is found that the conservation relation is better satisfied for those cases with a thinner separated region, without much dependence on the model used.


4th International Symposium on Physical Sciences in Space, ISPS-4 | 2011

Proposal of experimental setup on boiling two-phase flow on-orbit experiments onboard Japanese experiment module "kIBO"

Soumei Baba; Takashi Sakai; Kenichiro Sawada; Chisato Kubota; Y. A. Wada; Yasuhisa Shinmoto; Haruhiko Ohta; Hitoshi Asano; Osamu Kawanami; Koichi Suzuki; Ryoji Imai; Haruo Kawasaki; Kiyosumi Fujii; M Takayanagi; S Yoda


Transactions of the Japan Society of Mechanical Engineers. B | 1994

Fluid Behavior in Three-Dimensional Vane-Type Surface Tension Tandk under Reduced Gravity Condition.

Ryoji Imai; Toshikazu Yano; Shintaro Enya


Archive | 2000

TRANSPIRATION COOLING HEAT TRANSFER PROMOTION STRUCTURE OF TURBINE BLADE

Ryoji Imai; Shinsuke Matsuno; 良二 今井; 伸介 松野


Transactions of the Japan Society of Mechanical Engineers. B | 1997

A Study of Bubble Separation utilizing Centrifugal Force under a Reduced Gravity Condition

Ryoji Imai; Toshikazu Yano


Transactions of the Japan Society of Mechanical Engineers. B | 1994

Bubble Transfer by Electrostatic Force.

Ryoji Imai; Toshikazu Yano


JASMA : Journal of the Japan Society of Microgravity Application | 2011

Thermal Control System for Space Experiment on Two-Phase Boiling Flow-I : Analysis and Design of Condenser

Ryoji Imai; Koichi Suzuki; Haruo Kawasaki; Chungpyo Hong; Hiroya Ishizuka; Kiyosumi Fujii; Yasuhisa Shinmoto; Haruhiko Ohta


Archive | 2012

きぼう利用実験「沸騰二相流体ループにおける気液界面挙動と熱伝達特性」プロジェクトの進捗報告

清澄 藤井; 雅人 駒崎; 卓 栗本; 健一郎 澤田; 春夫 川崎; 康一 鈴木; 等 浅野; 治 河南; 良二 今井; 康久 新本; 治彦 大田; Kiyosumi Fujii; Masato Komasaki; Takashi Kurimoto; Kenichiro Sawada; Haruo Kawasaki; Koichi Suzuki; Hitoshi Asano; Osamu Kawanami; Ryoji Imai; Yasuhisa Shinmoto; Haruhiko Ohta


JASMA : Journal of the Japan Society of Microgravity Application | 2011

Thermal Control System for Space Experiment on Two-Phase Boiling Flow -II : Manufacture and Test of the Condenser system

Koichi Suzuki; Ryoji Imai; Chungpyo Hong; Haruo Kawasaki; Hiroya Ishizuka; Kiyosumi Fujii; Yasuhisa Shinmoto; Haruhiko Ohta

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Haruo Kawasaki

Japan Aerospace Exploration Agency

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Haruhiko Ohta

Tokyo University of Science

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Kiyosumi Fujii

Japan Aerospace Exploration Agency

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Koichi Suzuki

Tokyo University of Science

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Chungpyo Hong

Tokyo Metropolitan University

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