IRIE Tsukasa

J-GLOBAL         Last updated: May 30, 2018 at 13:57
 
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Name
IRIE Tsukasa
Affiliation
Kitakyushu National College of Technology
Section
Dept. of Mechanical Engineering
Job title
Professor
Degree
(BLANK)

Research Interests

 
 

Research Areas

 
 

Published Papers

 
入江司, 井上昌信
北九州工業高等専門学校研究報告(Web)   (50) 1‐4 (WEB ONLY)   Jan 2017
入江司, 井上昌信, 浅尾晃通, 小清水孝夫, 種健, 滝本隆, 田淵大介
北九州工業高等専門学校研究報告(Web)   47(47) 1-3 (WEB ONLY)-3   Jan 2014
入江司, 浅尾晃通, 井上昌信, 種健
北九州工業高等専門学校研究報告(Web)   (46) 1-2 (WEB ONLY)-2   Jan 2013   [Refereed]
入江司, 阿部雅二朗, 藤野俊和, 井上昌信
北九州工業高等専門学校研究報告(Web)   45(45) 1-4 (WEB ONLY)-4   Jan 2012
入江司, 井上昌信, 浅尾晃通, 種健, 阿部雅二朗, 藤野俊和
北九州工業高等専門学校研究報告(Web)   44(44) 9-13 (WEB ONLY)-13   Jan 2011
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
Transactions of the Japan Society of Mechanical Engineers. B   71(702) 405-411   Feb 2005
When the shock wave propagating along the straight circular tube reaches at the open end, the spherical shock wave is generated by the emission of a shock wave from an open end and the unsteady jet is formed near the open end behind the spherical ...
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
Transactions of the Japan Society of Mechanical Engineers. B   71(702) 412-419   Feb 2005
When the high-pressure gas is exhausted to the vacuum chamber from the nozzle exit, the underexpanded supersonic jet with the Mach disk is generally formed. The jet structure has been studied as a fundamental phenomenon of the supersonic fluid mec...
Tsukasa Irie, Hideo Kashimura, Toshiaki Setoguchi
Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B   71 412-419   Feb 2005
When the high-pressure gas is exhausted to the vacuum chamber from the nozzle exit, the underexpanded supersonic jet with the Mach disk is generally formed. The jet structure has been studied as a fundamental phenomenon of the supersonic fluid mec...
Tsukasa Irie, Hideo Kashimura, Toshiaki Setoguchi
Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B   71 405-411   Feb 2005
When the shock wave propagating along the straight circular tube reaches at the open end, the spherical shock wave is generated by the emission of a shock wave from an open end and the unsteady jet is formed near the open end behind the spherical ...
Tsukasa Irie, Tsuyoshi Yasunobu, Hideo Kashimura, Toshiaki Setoguchi
Theoretical and Applied Mechanics Japan   53 181-187   Dec 2004
When the high-pressure gas is exhausted to the vacuum chamber from the nozzle, an underexpanded supersonic jet is generally formed. The jet structure is complex, involving the interaction of the several flow features, making this a demanding probl...
Tsuyoshi Yasunobu, Takeshi Matsuoka, Tsukasa Irie, Hideo Kashimura, Toshiaki Setoguchi
Theoretical and Applied Mechanics Japan   52 103-108   Dec 2003
The numerical investigation of the self-induced flow oscillation caused by the interaction of a supersonic impinging jet is carried out in this paper. The self-induced flow oscillation occurs at the specific conditions and causes the noise problem...
T. Irie, T. Yasunobu, H. Kashimura, T. Setogushi
Journal of Thermal Science   12 132-137   Dec 2003
When the high-pressure gas is exhausted to the vacuum chamber from the nozzle, the underexpanded supersonic jet contained with the Mach disk is generally formed. The eventual purpose of this study is to clarify the unsteady phenomenon of the under...
Tsukasa Irie, Tsuyoshi Yasunobu, Hideo Kashimura, Toshiaki Setoguchi, Kazuyasu Matsuo
Journal of Thermal Science   12 245-249   Dec 2003
When the shock wave propagating in the straight circular tube reaches at the open end, the impulsive wave is generated by the emission of a shock wave from an open end, and unsteady pulse jet is formed near the open end behind the impulsive wave u...
Characteristics of Spherical Shock Wave and Circular Pulse Jet
Journal of Thermal Science   12(3) 245-249   2003
Characteristics of the Mack Disk in the Underexpanded Jet in which the Back Pressure Continuously Changes With Time
Journal of Thermal Science   12(2) 132-137   2003
IRIE Tsukasa, KASHIMURA Hideo, YASUNOBU Tsuyoshi, SETOGUCHI Toshiaki
Journal of the Visualization Society of Japan   22 255-258   Jul 2002
YASUNOBU Tsuyoshi, IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
Journal of the Visualization Society of Japan   22 351-354   Jul 2002
YASUNOBU Tsuyoshi, IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
Transactions of Visualization Society of Japan   22(1) 351-354   2002
The experimental investigation has been carried out using the thermo-sensitive liquid crystal sheet to obtain the two-dimensional temperature distribution. This study aims to build up the measuring system using the thermo-sensitive liquid crystal ...
IRIE Tsukasa, KASHIMURA Hideo, YASUNOBU Tsuyoshi, SETOGUCHI Toshiaki
Transactions of Visualization Society of Japan   22(1) 255-258   2002
When the shock wave propagating the straight circular tube reaches at the open end, the impulsive wave is generated by the emission of a shock wave from an open end and the unsteady pulse jet is formed near the open end behind the impulsive wave u...
ITO Hiroshi, HASEGAWA Mitsuhiko, IRIE Tsukasa, KATO Yoshio
Transactions of the Japan Society of Mechanical Engineers. C   51(462) 446-453   Feb 1985
トラッククレーンでクレーン作業を行なうときの,台車の前方安定度に関する研究である.第1報,後方安定度の研究において得た台車のシミュレーションモデルを発展させ,つり荷が降下する運動部分のモデルを追加し,前方へ転倒するクレーンの運動を理論的に解明した.その結果,従来未知であったトラッククレーンの機体数法諸元などと動的前方安定度の関係を明らかにし,設計段階で解析的に高い精度で予測できるようになった.
ITO Hiroshi, HASEGAWA Mitsuhiko, IRIE Tsukasa, KATO Yoshio
Transactions of the Japan Society of Mechanical Engineers. C   51(462) 454-458   Feb 1985
第2 報に続く前方安定度の研究である.前方の厳密なシミュレーションモデルに基づく解析方法は複雑で計算に時間がかかるため実用的でない.そこで,本論文では,厳密解とよく一致する近似モデルを設定し,つり荷降下時に急制動した場合に,クレーンがつり方向へ転倒する運動を理論的に解析した.その結果,簡便な式により前方安定度の許容限界値が予測できるようになり,クレーン機体の寸法諸元などの影響を明らかにした.

Conference Activities & Talks

 
井上昌信, 入江司
日本設計工学会研究発表講演会講演論文集   2016   
竹野康太, 矢野陽大, 福浦宏至, 入江司
日本設計工学会研究発表講演会講演論文集   2016   
入江司, 井上昌信
日本設計工学会研究発表講演会講演論文集   2016   
入江司, 井上昌信, 種健
日本設計工学会研究発表講演会講演論文集   May 2012   
UCHIDA Takeshi, MIYAUCHI Makoto, NAKAYAMA Hiroyasu, IRIE Tsukasa, HIRASHIMA Shigeki, ASAO Teruyuki
工学・工業教育研究講演会講演論文集   28 Jul 2006   
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
Fluids engineering conference ...   24 Nov 2004   
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
日本機械学会九州支部講演論文集   19 Mar 2004   
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
Fluids engineering conference ...   18 Sep 2003   
ノズルから噴出する不足膨張噴流は, 貯気圧と背圧の比によって膨脹波と圧縮波のセル状構造, バレル衝撃波が中心軸で交差する構造および中心軸と垂直な方向にマッハディスクが形成される構造となる。不足膨脹噴流に関する研究は, 実験的研究, 特性曲線法による解析および数値解析など多くなされているが, これらは圧力比が一定の定常噴流についての研究である。近年, 一様な流れの中に定在する斜め衝撃波の干渉形態に関するヒステリシス現象がわかってきた。しかし不足膨脹噴流の衝撃波の干渉に関するヒステリシス現象は...
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
日本機械学会九州支部講演論文集   14 Mar 2003   
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
講演論文集   10 Oct 2002   
IRIE Tsukasa, KASHIMURA Hideo, SETOGUCHI Toshiaki
講演論文集   10 Oct 2002   
KASHIMURA Hideo, IRIE Tsukasa, SETOGUCHI Toshiaki
講演論文集   21 Feb 2002   
IRIE Tsukasa
日本機械学会九州支部講演論文集   13 Mar 2000   

Research Grants & Projects

 
Hysteresis Phenomena of Shock Wave in Supersonic Jet
The Other Research Programs