FY2015

Reviewed Papers

2015/7/4-10: Large Eddy Simulation of Rocket Plume Acoustics using High Order Unstructured Grid Method
Takanori Haga, Seiji Tsutsumi(Research Unit Ⅲ), Soshi Kawai(University of Tokyo), Ryoji Takaki(Research Unit Ⅲ)
30th International Symposium on Space Technology and Science(ISTS 2015)
2015/5/13: Computational Study of the Rate Coefficients for the Reactions of N2 with CH3NHNH, CH3NNH2, and CH2NHNH2
Nozomu Kanno(Nagoya University), Hiroumi Tani, Yu Daimon(JEDI Center), Hiroshi Terashima(University of Tokyo), Norihiko Yoshikawa(Nagoya University), Mitsuo Koshi(JEDI Center)
Journal of Physical Chemistry A, American Chemical Society

Non-reviewed Papers, International and Domestic Conferences, etc.

2016/3/16,19: Numerical Modeling of Droplet Burning of Hypergolic Propellants
Hiroumi Tani, Yutaka Umemura, Yu Daimon (Research Unit III), Hiroshi Terashima(Hokkaido University), Mitsuo Koshi (Yokohama National University)
Asian Joint Conference on Propulsion and Power 2016(AJCPP 2016)
2016/3/16,19　: Study on Propellant Management Devices by Mesh-type Baffles
Shizuka Hamajima, Takehiro Himeno, Yasunori Sakuma, Toshinori Watanabe, Seiji Uzawa (University of Tokyo), Yutaka Umemura, Hideyo Negishi, Research Unit III), Keitaro Ishikawa (Mitsubishi Heavy Industries)
Asian Joint Conference on Propulsion and Power 2016(AJCPP 2016)
2016/3/16　: Validation and Verification of Numerical Prediction Method for Lift-off Acoustics of Launch
Seiji Tsutsumi (Research Unit III), Keita Terashima(JAXA)
Asian Joint Conference on Propulsion and Power 2016(AJCPP 2016)
2016/2/24　: Application of High-order Flux-reconstruction Method for Aerospace Simulation
Takanori Haga, Seiji Tsutsumi, Ryoji Takaki(Research Unit III), Soshi Kawai(Tohoku University)
Next Generation Transport Aircraft Workshop 2016
2016/1/5　: Application of Hybrid Turbulence Method to Transonic Flowfield of a Payload Fairing
Seiji Tsutsumi, Ryoji Takaki(Research Unit III), Shunsuke Koike(JAXA), Susumu Teramoto(University of Tokyo)
SciTech 2016, American Institute of Aeronautics and Astronautics(AIAA)
2016/1/4,8　: Interface-tracking Simulations of Droplet Vaporization and Burning of Hypergolic Propellant
Hiroumi Tani, Yutaka Umemura, Yu Daimon (Research Unit III), Hiroshi Terashima (University of Tokyo), Mitsuo Koshi (Yokohama National University)
SciTech 2016, American Institute of Aeronautics and Astronautics(AIAA)
2016/1/4,8　: Three-Dimensional Structures of Hypergolic Ignition Process and Flame Holding Mechanisms for Hydrazine/Nitrogen Dioxide Un-Like Doublet Impinging Gas Jets
Yu Daimon, Hiroumi Tani (Research Unit III), Hiroshi Terashima (University of Tokyo), Mitsuo Koshi (Yokohama National University)
SciTech 2016, American Institute of Aeronautics and Astronautics(AIAA)
2015/11/30　: Combustion Modeling Study for a GCH4/GOX single element combustion chamber : unsteady simulations
Hiroshi Ishihara(University of Tokyo), Yu Daimon(Research Unit III)
Proceedings of Summer Program 2015, Technological foundations for the design of thermally and mechanically highly loaded components of future space transportation systems
2015/11/30　: Comparison of different modeling approaches for CFD simulations of a single-element GCH4/GOX rocket combustor
Yu Daimon(Research Unit III), Hiroshi Terashima(University of Tokyo), Hideyo Negishi(Research Unit III), Oskar Haidn(Technische Universität München)
Proceedings of Summer Program 2015, Technological foundations for the design of thermally and mechanically highly loaded components of future space transportation systems
2015/11/30　: Combustion Modeling Study for a GCH4/GOX single element combustion chamber : Steady State Simulation and Validations
C. Rothy, O. Haidn(Technische Universität München), H. Riedmannz, B. Ivancicz(Airbus DS GmbH), D. Maestro, B. Cuenot(CERFACS), L. Selle(IMFT), Yu Daimon(Research Unit III), A. Chemnitz(Technische Universität München), R. Keller(Universität Stuttgart), J. Zips, G. Frank, H. Muller(Universität der Bundeswehr München)
Proceedings of Summer Program 2015, Technological foundations for the design of thermally and mechanically highly loaded components of future space transportation systems
2015/9/15-17　: Recent R&D Outcomes in JAXA using CFD++
Taro Shimizu(Research Unit Ⅲ)
Metacomp Symposium 2015, Metacomp. Tech. Inc.
2015/8/7　: Effects of Droplet Size on Hypergolic Combustion of Hydrazine Spray
Hiroumi Tani(Research Unit Ⅲ), Hiroshi Terashima(University of Tokyo), Ryoichi Kurose, Tomoaki Kitano(Kyoto University),Mitsuo Koshi(Yokohama National University), Yu Daimon(Research Unit Ⅲ)
International Colloquium on the Dynamics of Explosions and Reactive Systems, Institute for Dynamics of Explosions and Reactive Systems
2015/7/27　: Numerical Modeling of Boiling Flow in a Cryogenic Propulsion System
Yutaka UMEMURA(Research Unit Ⅲ), Takehiro HIMENO(The University of Tokyo), Kiyoshii KINEFUCHI(Research Unit Ⅳ), Naoki TANI, Hideyo NEGISHI(Research Unit Ⅲ), Hiroaki KOBAYASHI(Next Generation Aeronautical Innovation Hub Center,JAXA), Katsuhide OHIRA(Tohoku Uversity), Osamu FUKASAWA(Ryoyu System Co.,)
AIAA Propulsion and Energy 2015, AIAA
2015/7/27　: Regenerative Cooling Performance Analysis of the LE-X Engine Combustion Chamber
Hideyo Negishi,Yu Daimon(Research Unit Ⅲ), Nobuyuki Negoro, Akihide Kurosu(Space Technorogy Directrate I,JAXA)
AIAA Propulsion and Energy 2015, AIAA
2015/7/7　: Numerical Aeroacoustics Analysis of a Scaled Solid Jet Impinging on Flat Plate with Exhaust Hole
Seiji Tsutsumi, Ryoji Takaki(Research Unit Ⅲ), Hiroshi Ikaida(Epsilon Rocket Project Team), Keita Terashima(University of Tokyo)
30th International Symposium on Space Technology and Science(ISTS 2015)
2015/6/29-7/3　: Numerical Analysis of Combustion for Droplet of Hydrazine
Mikiro Motoe(Research Unit Ⅲ)
EUCASS 2015, EUCASS
2015/6/22　: Automated Massively Refinement Technique for Multi-block Structured Grids Based on NURBS Volume
Hiroshi Koizumi,Seiji Tsutsumi,Ryoji Takaki(Research Unit Ⅲ),Kazuomi Yamamoto(FQUROH Project Team),Hiroyuki Ito,Masaharu Abe(Ryoyu Systems),Yosuke Matsumura(Mizuho Information & Research Insititute)
AVIATION 2015, AIAA
2015/6/7-11　: DUAL TIME STEPPING METHOD FOR CHEMICAL KINETICS ODES
Eiji Shima, Youhi Morii(Research Unit Ⅲ)
Ninth Mediterranean Combusion Symposium, Combistion Institute
2015/6/3-5　: Comparison of Dynamic Adaptive Sampling Methods for Quantitative Risk Analysis
K.Fujimoto(JEDI Center), K.Shimoyama(TOHOKU University), H.Negishi(JEDI Center)
2nd Frontiers in Computational Physics Conference: Energy Sciences　，Elsevier
2015/6/3-5　: Dissociation Reaction of CH2NNH2: Implications for the Pyrolysis of CH3NHNH2
Kanno Nozomu (Nagoya University), Tani Hiroumi, Daimon Yu (Research Unit Ⅲ), Terashima Hiroshi (University of Tokyo), Yoshikawa Norihiko (Nagoya University), Koshi Mitsuo (Universsity of Tokyo)
31th Symposium on Chemical Kinetics and Dynamics
2015/5/18,20　: Affordable High-reliability Realization Approach in Liquid Rocket Engine Development for New National Flagship Launch Vehicle
Kaname Kawatsu, Hajime Taguchi (JEDI Center), Akihide Kurosu, Teiu Kobayash, Koichi Okita (JAXA), Akira Nakajima, Nobuhiko Kumada, Akira Ogawara, Hiroyasu Manako (Mitsubishi Heavy Industories)
TRISMAC2015
2015/4/19-22　: Three-Dimensional Structures of Hypergolic Ignition Process for Hydrazine/Nitrogen Dioxide Un-like Doublet Impinging Gas Jets
Y.Daimon, H.Tani (Research Unit Ⅲ), H.Terashima,M.koshi (University of Tokyo)
15th International Conference on Numerical Combustion　，SIAM
2015/4: Oscillatory combustion in a sub-scale liquid rocket chamber
T. Shimizu, Y. Morii（Research Unit Ⅲ）, Y. Mizobuchi（Numerial Simulation Research Unit, JAXA）, Nunome Yoshio,Takeo Tomita（Research Unit Ⅳ, JAXA）, Hideto Kawashima（H3 Project team, JAXA）, Manabu Hishida (Ryouyu systems)
Numerical Combustion, Apr. 2015, Avignon, France.