Hiroshi Terashima

J-GLOBAL         Last updated: Dec 18, 2019 at 17:29
 
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Name
Hiroshi Terashima
Nickname
htera
E-mail
hteraeng.hokudai.ac.jp
Affiliation
Hokkaido University
Section
Faculty of Engineering
Job title
Associate Professor
Degree
Ph.D.
Research funding number
20415235

Research Areas

 
 

Academic & Professional Experience

 
Dec 2015
 - 
Today
Associate Professor, Faculty of Engineering, Hokkaido University
 
Apr 2013
 - 
Nov 2015
Project Associate Professor, School of Engineering, University of Tokyo
 
Apr 2011
 - 
Mar 2013
Research Associate, School of Engineering, University of Tokyo
 
Apr 2009
 - 
Mar 2011
Aerospace Project Researcher, JEDI, JAXA
 
Apr 2007
 - 
Mar 2009
Research Scientist, Mechanical Engineering Department, Worcester Polytechnic Institute
 

Published Papers

 
Terashima Hiroshi, Matsugi Akira, Koshi Mitsuo
COMBUSTION AND FLAME   203 204-216   May 2019   [Refereed]
Daiki Muto, Hiroshi Terashima, Nobuyuki Tsuboi
Transactions of the Japan Society for Aeronautical and Space Sciences   62 203-212   Jan 2019   [Refereed]
© 2019 The Japan Society for Aeronautical and Space Sciences. The effects of a recess on co-flowing planar jets under supercritical pressure are numerically studied. Two-dimensional hybrid LES/RANS simulations are performed in a wide range of rece...
A. Razmi, M. Taeibi-Rahni, H. R. Massah, H. Terashima, H. Moezzi
Journal of Applied Fluid Mechanics   12 631-645   Jan 2019   [Refereed]
© 2019 Isfahan University of Technology. A front tracking/ghost fluid method was used to simulate fluid interfaces in a shock-bubble interaction problem. The method captures fluid interfaces, using explicit front-tracking and defines interface con...
Hiroumi Tani, Hiroshi Terashima, Yu Daimon, Mitsuo Koshi, Ryoichi Kurose
Combustion Science and Technology   190 515-533   Mar 2018   [Refereed]
© 2017 Taylor & Francis. Unsteady simulations of hydrazine (N 2 H 4 ) sprays in nitrogen tetroxide (NTO, NO 2 -N 2 O 4 ) streams were conducted to explore the hypergolic combustion in bipropellant thrusters. The Navier–Stokes equations were solv...
D Deb, MA Uddin, H Terashima, N Oshima
Journal of Scientific Research   10(2) 117-131   2018   [Refereed]
Ohashi Tatsushi, Takahashi Yusuke, Terashima Hiroshi, Oshima Nobuyuki
JOURNAL OF FLUID SCIENCE AND TECHNOLOGY   13(3)    2018   [Refereed]
Hiroshi Terashima, Akira Matsugi, Mitsuo Koshi
Combustion and Flame   184 324-334   Jan 2017   [Refereed]
© 2017 The Combustion Institute The present study deals with the mechanisms for the hot-spot formation and pressure wave development associated with end-gas autoignition during knocking combustion of n-heptane/air mixture. The discussion is based ...
Akira Matsugi, Hiroshi Terashima, Hiroshi Terashima
Combustion and Flame   179 238-241   Jan 2017   [Refereed]
© 2017 The Combustion Institute The diffusive-thermal effect plays an important role in the intrinsic instability of premixed flames. A two-dimensional direct numerical simulation of the propagation of premixed hydrogen–air flames was performed us...
Youhi Morii, Hiroshi Terashima, Mitsuo Koshi, Taro Shimizu, Eiji Shima
Journal of Computational Physics   322 547-558   Oct 2016   [Refereed]
© 2016 Elsevier Inc. We herein propose a fast and robust Jacobian-free time integration method named as the extended robustness-enhanced numerical algorithm (ERENA) to treat the stiff ordinary differential equations (ODEs) of chemical kinetics. Th...
Soshi Kawai, Hiroshi Terashima, Hideyo Negishi
Journal of Computational Physics   300 116-135   Nov 2015   [Refereed]
© 2015 Elsevier Inc.. This paper addresses issues in high-fidelity numerical simulations of transcritical turbulent flows at supercritical pressure. The proposed strategy builds on a tabulated look-up table method based on REFPROP database for an ...
Nozomu Kanno, Nozomu Kanno, Hiroumi Tani, Yu Daimon, Hiroshi Terashima, Norihiko Yoshikawa, Mitsuo Koshi
Journal of Physical Chemistry A   119 7659-7667   Jul 2015   [Refereed]
© 2015 American Chemical Society. The reactions of NO<inf>2</inf> with cis-/trans-CH<inf>3</inf>NHNH, CH<inf>3</inf>NNH<inf>2</inf> and CH<inf>2</inf>NHNH<inf>2</inf> have been studied theoretically by quantum chemical calculations and steady-stat...
Hiroshi Terashima, Mitsuo Koshi
Combustion and Flame   162 1944-1956   May 2015   [Refereed]
© 2014 The Combustion Institute. A knocking combustion modeled using a one-dimensional constant volume reactor is simulated in a manner of direct numerical simulations, in which large detailed chemical kinetic mechanisms for two premixed gases, n-...
Youhi Morii, Hiroshi Terashima, Mitsuo Koshi, Taro Shimizu
Journal of Loss Prevention in the Process Industries   34 92-99   Mar 2015   [Refereed]
© 2015 Elsevier Ltd. A numerical simulation of the spontaneous ignition of high-pressure hydrogen in a duct with two obstacles on the walls is conducted to explore the spontaneous ignition mechanisms. Two-dimensional rectangular ducts are adopted,...
Hiroshi Terashima, Youhi Morii, Mitsuo Koshi
International Journal of Energetic Materials and Chemical Propulsion   14 177-196   Jan 2015   [Refereed]
© 2015 by Begell House, Inc. A robust explicit time integration method for stiff chemical reaction equations is proposed and applied to zero-dimensional ignition and one-dimensional combustion flow problems. The proposed method based on a multi-ti...
Hiroumi Tani, Hiroshi Terashima, Mitsuo Koshi, Yu Daimon
Proceedings of the Combustion Institute   35 2199-2206   Jan 2015   [Refereed]
© 2014 The Combustion Institute. Published by Elsevier Inc. All rights reserved. Hydrazine (N2H4)/nitrogen tetroxide (NTO) co-flowing plane jets were simulated to explore the hypergolic ignition processes and flame structures in N2H4/NTO bipropell...
Hiroumi Tani, Hiroshi Terashima, Yu Daimon, Mitsuo Koshi
International Journal of Energetic Materials and Chemical Propulsion   14 71-84   Jan 2015   [Refereed]
© 2015 by Begell House, Inc. Hydrazine (N<inf>2</inf>H<inf>4</inf>)/nitrogen tetroxide (NTO) co-flowing jets were simulated to explore the hypergolic ignition processes in N<inf>2</inf>H<inf>4</inf>/NTO bipropellant thrusters. The Navier–Stokes eq...
森井雄飛, 寺島洋史, 越光男, 清水太郎
日本燃焼学会誌   56(176) 156-165   May 2014   [Refereed]
Hiroshi Terashima, Mitsuo Koshi, Chika Miwada, Toshio Mogi, Ritsu Dobashi
International Journal of Hydrogen Energy   39 6013-6023   Apr 2014   [Refereed]
A two-dimensional (2-D) simulation of spontaneous ignition of high-pressure hydrogen in a length of duct is conducted to explore ignition mechanisms. The present study adopts a 2-D rectangular duct and focuses on effects of the initial diaphragm s...
Nozomu Kanno, Hiroshi Terashima, Yu Daimon, Norihiko Yoshikawa, Mitsuo Koshi
International Journal of Chemical Kinetics   46 489-499   Jan 2014   [Refereed]
The kinetics and mechanisms of H atom abstraction reactions from CH 3NHNH2 by NO2 (R1) and related reactions have been investigated theoretically by using ωB97X-D and CCSD(T)-F12 quantum chemical calculations and the steady-state unimolecular mast...
Yu Daimon, Hiroshi Terashima, Mitsuo Koshi
Journal of Propulsion and Power   30 707-716   Jan 2014   [Refereed]
A detailed chemical kinetic mechanism for hypergolic ignition of N 2H4 in a N2O4-NO2 gas mixture has been constructed. In this mechanism, the hypergolic ignition is mainly caused by the sequential reactions of H atom abstraction from N 2Hm by NO2:...
Hiroshi Terashima, Soshi Kawai, Mitsuo Koshi
Computers and Fluids   88 484-495   Dec 2013   [Refereed]
An interface-capturing method using a high-order central difference scheme is presented for simulations of compressible multicomponent flows. The present method adds consistent numerical diffusion terms to robustly capture interface discontinuitie...
寺島洋史, 越光男
日本燃焼学会誌   55(174) 411-421   Nov 2013   [Refereed]
Chihiro Inoue, Mitsuo Koshi, Hiroshi Terashima, Takehiro Himeno, Toshinori Watanabe
Science and Technology of Energetic Materials   74 106-111   Nov 2013   [Refereed]
The physics behind the beauty of sparkling fireworks has not been clarified yet due to a lack of detailed visualization results. In the present study, atomization process in sparkling fireworks is elucidated by using a high-speed video camera. In ...
Hiroshi Terashima, Mitsuo Koshi
Journal of Propulsion and Power   29 1328-1336   Nov 2013   [Refereed]
Two-dimensional planar and three-dimensional round nitrogen jets under supercritical pressures are simulated with a wide range of conditions to explore their unique characteristics. A high-order method using a sixth-order compact scheme is applied...
Hiroshi Terashima, Mitsuo Koshi
Computers and Fluids   85 39-46   Oct 2013   [Refereed]
This study presents a strategy for simulations of cryogenic single-species jets under supercritical pressure conditions. In this strategy, a pressure evolution equation is introduced and numerical diffusion terms are consistently constructed in or...
INOUE Chihiro, KOSHI Mitsuo, TERASHIMA Hiroshi, HIMENO Takehiro, WATANABE Toshinori
Science and technology of energetic materials : Journal of the Japan Explosives Society   74(3) 106-111   Aug 2013   [Refereed]
Yu Daimon, Hiroshi Terashima, Mitsuo Koshi
Science and Technology of Energetic Materials   74 17-22   Jul 2013   [Refereed]
Hydrazine (N2H4) has a unique characteristic inducing hypergolic ignition even at very low temperatures with nitrogen dioxide (NO2). In order to understand the chemical kinetic origin of this hypergolic nature, thermochemical data (heat of formati...
Hiroshi Terashima, Mitsuo Koshi
Journal of Computational Physics   231 6907-6923   Aug 2012   [Refereed]
This study proposes an approach for simulations of cryogenic fluid mixing under supercritical pressures using high-order schemes. In this approach, we introduce a pressure evolution equation and consistently construct numerical diffusion terms to ...
Taku Nonomura, Seiichiro Morizawa, Hiroshi Terashima, Shigeru Obayashi, Kozo Fujii
Journal of Computational Physics   231 3181-3210   Apr 2012   [Refereed]
A weighted compact nonlinear scheme (WCNS) is applied to numerical simulations of compressible multicomponent flows, and four different implementations (fully or quasi-conservative forms and conservative or primitive variables interpolations) are ...
Hiroshi Terashima, Soshi Kawai, Nobuhiro Yamanishi
AIAA Journal   49 2658-2672   Dec 2011   [Refereed]
A high-resolution methodology using a high-order compact differencing scheme with localized artificial diffusivity is introduced with the aim of simulating jet mixing under supercritical pressure environments. The nonlinear localized artificial di...
Soshi Kawai, Hiroshi Terashima
International Journal for Numerical Methods in Fluids   66 1207-1225   Aug 2011   [Refereed]
A simple methodology for a high-resolution scheme to be applied to compressible multicomponent flows with shock waves is investigated. The method is intended for use with direct numerical simulation or large eddy simulation of compressible multico...
Hiroshi Terashima, Grétar Tryggvason
Computers and Fluids   39 1804-1814   Dec 2010   [Refereed]
A front-tracking method for compressible multi-fluid flows is presented, where marker points are used both for tracking fluid interfaces and also for constructing the Riemann problem on the interfaces. The Riemann problem between the two fluid pha...
Hiroshi Terashima, Grétar Tryggvason
Journal of Computational Physics   228 4012-4037   Jun 2009   [Refereed]
A front-tracking/ghost-fluid method is introduced for simulations of fluid interfaces in compressible flows. The new method captures fluid interfaces using explicit front-tracking and defines interface conditions with the ghost-fluid method. Sever...
Hiroshi Terashima, Kozo Fujii
AIAA Journal   45 237-246   Jan 2007   [Refereed]
Transonic and supersonic flutter characteristics of a delta wing configuration with external stores were computationally simulated, and the aerodynamic influence of the stores on the flutter characteristics was investigated. Delta wings with one a...
TERASHIMA Hiroshi, FUJII Kozo
Transactions of the Japan Society of Mechanical Engineers B   71(712) 2856-2863   Dec 2005   [Refereed]
One criterion that determines time stepping size in the implicit time integration method is given for accurate and effective transonic flutter simulations. Transonic flows over two-dimensional forced oscillating air foils with several reduced freq...

Misc

 
寺島洋史
日本燃焼学会誌   59(189) 149‐150   Aug 2017
越光男, 寺島洋史, 谷洋海, 大門優
衝撃波シンポジウム講演論文集(CD-ROM)   2016 ROMBUNNO.TOKUベTSUKOEN II   2017
森井雄飛, 寺島洋史
日本ガスタービン学会誌   44(2) 96‐101   Mar 2016
MORII Youhi, TERASHIMA Hiroshi, KOSHI Mitsuo, SHIMIZU Taro, SHIMA Eiji
Journal of Japan Society of Fluid Mechanics   34(2) 131-135   Apr 2015
TERASHIMA Hiroshi, KOSHI Mitsuo
Journal of Japan Society of Fluid Mechanics   31(4) 351-356   Aug 2012
井上 智博, 寺島 洋史, 根岸 秀世
Aeronautical and space sciences Japan   58(677) 185-191   Jun 2010
KU Katharine
Journal of the Japan Society for Computational Engineering and Science   9(2) 900-902   Apr 2004

Conference Activities & Talks

 
Shun Murakami, Hiroshi Terashima, Nobuyuki Oshima
AIAA Scitech 2019 Forum   1 Jan 2019   
© 2019 by Timothy K. Minton. Published by the American Institute of Aeronautics and Astronautics, Inc. A computational study is performed for exploring flow and flame dynamics of a high-pressure hydrogen/oxygen coflow jet with the effects of post ...
Takahide Araki, Daiki Muto, Hiroshi Terashima, Nobuyuki Tsuboi
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting   1 Jan 2017   
© 2017 by Rolls-Royce North America Holdings Inc. Three-dimensional numerical simulations of coaxial nitrogen jet mixing under supercritical pressures are performed with an emphasis on the effects of pressure on the mixing. The results show that t...
藤田晴彦, 伊藤祐太朗, 山田眞平, 下栗大右, 佐藤伴音, 寺島洋史, 河野通治, 本田雄哉, 植木義治, 横畑英明
日本伝熱シンポジウム講演論文集(CD-ROM)   2017   
榎尚也, 松永学, 高橋裕介, 寺島洋史, 大島伸行
流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM)   2017   
大橋達志, 松永学, 高橋裕介, 寺島洋史, 大島伸行
流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM)   2017   
寺島洋史, 松木亮
燃焼シンポジウム講演論文集   26 Nov 2016   
佐藤伴音, 寺島洋史, 大島伸行
燃焼シンポジウム講演論文集   26 Nov 2016   
H. Terashima, Y. Daimon
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016   1 Jan 2016   
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. A two-dimensional detailed numerical simulation is performed for combustion flow field of a GCH4/GOX single injector using detailed chemical kinetics with t...
Hiroumi Tani, Yutaka Umemura, Yu Daimon, Hiroshi Terashima, Mitsuo Koshi
54th AIAA Aerospace Sciences Meeting   1 Jan 2016   
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, All rights reserved. The vaporization and burning of the N 2 H 4 and NTO droplets were simulated with the interface-tracking method to accurately explore the auto-ignition proc...
Daiki Muto, Hiroshi Terashima, Nobuyuki Tsuboi
54th AIAA Aerospace Sciences Meeting   1 Jan 2016   
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Three-dimensional numerical simulations of cryogenic coaxial jets under supercritical pressure are performed with flushed and recessed injectors to investig...
Yu Daimon, Hiroumi Tani, Hiroshi Terashima, Mitsuo Koshi
54th AIAA Aerospace Sciences Meeting   1 Jan 2016   
© 2016 by the American Institute of Aeronautics, and Astronautics, Inc. All rights reserved. Hydrazine (N 2 H 4 )/nitrogen dioxide (NO 2 ) un-like doublet impinging gas jets were simulated to explore the hypergolic ignition processes in a N 2 H 4 ...
寺島洋史, 大門優
日本機械学会熱工学コンファレンス講演論文集(CD-ROM)   2016   
武藤大貴, 武藤大貴, 寺島洋史, 坪井伸幸
数値流体力学シンポジウム講演論文集(CD-ROM)   2016   
Daiki Muto, Nobuyuki Tsuboi, Hiroshi Terashima
53rd AIAA Aerospace Sciences Meeting   1 Jan 2015   
© 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. The effects of the injector geometries on co-flowing planar cryogenic jet mixings under a supercritical condition are numerically investigated. The present...
Hiroumi Tani, Hiroshi Terashima, Ryoichi Kurose, Tomoaki Kitano, Mitsuo Koshi, Yu Daimon
53rd AIAA Aerospace Sciences Meeting   1 Jan 2015   
© 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Hydrazine (N 2 H 4 ) spray/gaseous nitrogen tetroxide (NTO) co-flowing jets were simulated to explore the hypergolic combustion flows in N 2 H 4 /NTO bipro...
Hiroshi Terashima, Mitsuo Koshi
52nd Aerospace Sciences Meeting   1 Jan 2014   
© 2014, American Institute of Aeronautics and Astronautics Inc. All rights reserved. Three-dimensional simulations for nitrogen/hydrogen mixing of a shear coaxial injector under supercritical pressures are conducted in order to investigate their m...
Akira Kikusato, Kazuya Kogo, Beini Zhou, Kusaka Jin, Yasuhiro Daisho, Kiyotaka Sato, Hidefumi Fujimoto, Hiroshi Terashima, Youhi Morii
SAE Technical Papers   1 Jan 2014   
Copyright © 2014 SAE International. The objective of the present study is to analyze soot formation in diesel engine combustion by using multi-dimensional combustion simulations with a parallelized explicit ODE solver. Parallelized CHEMEQ2 was use...
Youhi Morii, Hiroshi Terashima, Mitsuo Koshi, Taro Shimizu, Eiji Shima
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014   1 Jan 2014   
© 2014 by authors. Published by the American Institute of Aeronautics and Astronautics, Inc. A simple yet robust and fast time integration method is proposed for efficiently solving stiff chemical kinetic ordinary differential equations. The propo...
Daiki Muto, Nobuyuki Tsuboi, Hiroshi Terashima
52nd Aerospace Sciences Meeting   1 Jan 2014   
© 2014, American Institute of Aeronautics and Astronautics Inc. All rights reserved. Effects of recess on the mixing of the cryogenic coaxial jet under supercritical conditions were numerically investigated. Recessed injectors have been applied as...
Yu Daimon, Hiroshi Terashima, Mitsuo Koshi
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013   19 Aug 2013   
A detailed chemical kinetic mechanism for hypergolic ignition of N2H4/NO2 gas mixture at low temperatures has been constructed. In this mechanism, the hypergolic ignition is caused by following sequential reactions of H atom abstraction from N2Hm ...

Research Grants & Projects

 
Ministry of Education, Culture, Sports, Science and Technology: Grants-in-Aid for Scientific Research(基盤研究(B))
Project Year: 2011 - 2013    Investigator(s): Nobuyuki TSUBOI
The numerical and experimental studies on the cryogenic flow under the supercritical pressure are performed in order to understand the thermodynamic characteristics and fluid dynamics. The averaged density distributions of the mono-axial nitrogen ...
Ministry of Education, Culture, Sports, Science and Technology: Grants-in-Aid for Scientific Research(基盤研究(B))
Project Year: 2011 - 2013    Investigator(s): Mitsuo KOSHI
Reactive flow analysis for complex system such as automobile engine knocking and vibratory combustion in gas turbine needs fluid dynamic simulation coupled with detailed chemical kinetics. Because of very large numbers of chemical species involved...
Ministry of Education, Culture, Sports, Science and Technology: Grants-in-Aid for Scientific Research(若手研究(B))
Project Year: 2011 - 2012    Investigator(s): Hiroshi TERASHIMA
A front tracking method for compressible multi-fluid flows is presented where marker points are used both for tracking fluid interfaces and also for constructing the Riemann problem on the interfaces. The Riemann problem between two fluid phases (...