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Featured researches published by Daiki Muto.


54th AIAA Aerospace Sciences Meeting | 2016

Numerical Simulation of Jet Mixing in a Recessed Coaxial Injector at Supercritical Pressure

Daiki Muto; Hiroshi Terashima; Nobuyuki Tsuboi

Three-dimensional numerical simulations of cryogenic coaxial jets under supercritical pressure are performed with flushed and recessed injectors to investigate the effect of a recess on the coaxial mixing. A hybrid ILES/RANS method is applied to simulate wallbounded injectors and a recessed region. The recessed injector enhances the density decay and the temperature increase on the central axis, indicating the improvement of mixing compared with the flushed injector. However, the mixing improvement by the recess is not significant in the present conditions. The recess also induces distinct vortex rings around the outer jet. The power spectra of the velocity fluctuations also demonstrated that the low-frequency velocity fluctuations are clearly induced by the recess which frequency corresponds to the large vortex structures.


53rd AIAA Aerospace Sciences Meeting | 2015

Effects of Injector Geometry on Co-Flowing Planar Jet Mixings under Supercritical Pressures

Daiki Muto; Nobuyuki Tsuboi; Hiroshi Terashima

The effects of the injector geometries on co-flowing planar cryogenic jet mixings under a supercritical condition are numerically investigated. The present study focuses the recess of the coaxial injector which is widely applied in practical liquid rocket engines. The present numerical method applies an ILES/RANS hybrid method to simulate the jet mixing in the wall-bounded recessed region. As a validation of the present method, a mono-planar jet and a round jet simulations are carried out, and the results agree well with an experimental result. To examine the effects of the recess length on the coaxial injections, two-dimensional co-planar jet simulations at the supercritical pressure are performed in three recess lengths. The recessed cases show the strong flapping motions of the high densty jet, and as a result, the injected fluids are mixed well compared with the case without the recess. While there is a small difference on the potential core length between the cases without the recess and the shorter recess, the longer recess case largely shortens the jet core.


55th AIAA Aerospace Sciences Meeting | 2017

Three-dimensional Numerical Simulation on Dispersion Process of Unsteady High Pressure Hydrogen Jet Flow

Nobuyuki Tsuboi; Keisuke Fujimoto; Daiki Muto; Makoto Asahara


55th AIAA Aerospace Sciences Meeting | 2017

Numerical Simulation for Effects of Pressure on Cryogenic Coaxial Jet under Supercritical Pressure

Takahide Araki; Daiki Muto; Hiroshi Terashima; Nobuyuki Tsuboi


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2016

Characteristics of Jet-Mixing at Supercritical Pressure: Effects of Recess Length and Post Height

Daiki Muto; Hiroshi Terashima; Nobuyuki Tsuboi


The Proceedings of the Fluids engineering conference | 2016

Three-Dimensional Numerical Simulation on Dispersion Process of High Pressure Hydrogen Jet

Keisuke Fujimoto; Daiki Muto; Nobuyuki Tsuboi; Makoto Asahara


The Proceedings of Mechanical Engineering Congress, Japan | 2016

Numerical Simulations of Jet/Free-stream Interaction Mechanism on Liquid Rocket Tank Destruction

Toshihiro Iwasa; Daiki Muto; Keiichiro Fujimoto; Nobuyuki Tsuboi


The Proceedings of Conference of Kyushu Branch | 2016

D-08 Numerical Simulations of Jet/Free-stream Interaction Structures on Liquid Rocket Tank Destruction

Toshihiro Iwasa; Daiki Muto; Keiichiro Fujimoto; Nobuyuki Tsuboi


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2014

Numerical Study of Real Gas Effects on Shock Tube Problems at Supercritical Conditions

Daiki Muto; Nobuyuki Tsuboi; Hiroshi Terashima


The Proceedings of Conference of Kyushu Branch | 2014

802 Numerical Study of Injector Geometry Effects on Cryogenic Coaxial Jet under Supercritical Conditions

Daiki Muto; Nobuyuki Tsuboi; Hiroshi Terashima

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Nobuyuki Tsuboi

Kyushu Institute of Technology

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Keiichiro Fujimoto

Japan Aerospace Exploration Agency

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Makoto Asahara

Aoyama Gakuin University

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