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Reaction mechanism reduction for ethylene-fueled supersonic combustion CFD

CEAS space journal, 2023-11, Vol.15 (6), p.845-866

2023

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Unsteady Numerical Analysis of a Dual-Mode Scramjet Combustor with a Cavity

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2023, Vol.66(4), pp.103-117

2023

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Numerical Study of Restricted Shock Separation in a Compressed Truncated Perfect Nozzle

AIAA journal, 2006-03, Vol.44 (3), p.576-584

2006

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Flush Air Data Sensing System for a Sharp-Nosed Hypersonic Vehicle with Curved-Wedge Forebody

AIAA journal, 2020-11, Vol.58 (11), p.4819-4831

2020

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Physical Insight into Fuel/Air Mixing with Hypermixer Injectors for Scramjet Engines

Journal of propulsion and power, 2015-09, Vol.31 (5), p.1423-1435

2015

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Applications of unstructured hybrid grid method to high-Reynolds number viscous flows

International journal for numerical methods in fluids, 1999-09, Vol.31 (1), p.97-111

1999

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Calibration of Oxygen Atom Mass Fraction in High Enthalpy Shock Tunnel Flow Based on Shock Stand-off Distance Measurement

TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, 2011, Vol.77(774), pp.227-236

2011

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Numerical Study on Combustor Flow-Path Design for a Scramjet Flight Experiment

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2021, Vol.19 (3), p.415-423

2021

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Arrangement of Rocket Engine Location in a Combined Cycle Engine

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2019, Vol.17 (2), p.165-174

2019

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Force Measurement of Large-scale Scramjet Model within Short Test Duration

Transactions of the Japan Society of Mechanical Engineers Series B, 2005/06/25, Vol.71(706), pp.1596-1602

2005

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System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2014-01, Vol.12 (ists29), p.Pa_91-Pa_99

2014

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Some Aspects on Hydrocarbon-fueled RBCC Engines for a TSTO Launch Vehicle

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2016, Vol.14 (ists30), p.Po_1_1-Po_1_8

2016

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Formation of dot arrays with a pitch of 20 nm × 20 nm for patterned media using 30 keV EB drawing on thin calixarene resist

Nanotechnology, 2008-01, Vol.19 (2), p.025301-025301

2008

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Formation of dot arrays with a pitch of 20nm X 20nm for patterned media using 30keV EB drawing on thin calixarene resist

Nanotechnology, 2008-01, Vol.19 (2), p.025301 (4)-025301 (4)

2008

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Free-Flight Testing in the Gas-Driven Two-Stage Light Gas Gun HEK-G

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2012, Vol.10 (ists28), p.Tr_41-Tr_45

2012

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Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method

JSME International Journal Series B Fluids and Thermal Engineering, 2000/08/15, Vol.43(3), pp.407-413

2000

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Simulation of 3D Shock Wave/Turbulent Boundary Layer Interactions by Hybrid Grid Method

Transactions of the Japan Society of Mechanical Engineers Series B, 1998/11/25, Vol.64(627), pp.3669-3674

1998

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Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method

Transactions of the Japan Society of Mechanical Engineers Series B, 1999/05/25, Vol.65(633), pp.1513-1519

1999

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Airframe- Configuration Effect on Condition of Airflow to Engine in Hypersonic Flow

Journal of propulsion and power, 2007-09, Vol.23 (5), p.1134-1136

2007

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衝撃波離脱距離計測による高温衝撃風洞流れの酸素原子の検定

日本機械学会論文集Ｂ編, 2011, Vol.77(774), pp.227-236

2011

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214 Numerical Analysis of an Ethanol Fueled RBCC Engine

The Proceedings of The Computational Mechanics Conference, 2013, Vol.2013.26, p.214-1-214-2

2013

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Force Measurement of Large-scale Scramjet Model within Short Test Duration

Nihon Kikai Gakkai rombunshuu. B hen, 2005-06, Vol.17 (6), p.1596-1602

2005

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Considerations on Mixing and Combustion of a Scramjet Engine

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2002, Vol.50(576), pp.22-22

2002

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Considerations on Mixing and Combustion of a Scramjet Engine. Transition Processes from Weak to Intensive Combustion Mode

Nihon Kōkū Uchū Gakkai ronbunshū, 2002, Vol.50 (576), p.22-29

2002

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Evaluation of Scramjet Testing Technology in the High Enthalpy Shock Tunnel HIEST

Nihon Kikai Gakkai rombunshuu. B hen, 2004-11, Vol.16 (11), p.2758-2767

2004

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Reaction mechanism reduction for ethylene-fueled supersonic combustion CFD

Unsteady Numerical Analysis of a Dual-Mode Scramjet Combustor with a Cavity

Numerical Study of Restricted Shock Separation in a Compressed Truncated Perfect Nozzle

Flush Air Data Sensing System for a Sharp-Nosed Hypersonic Vehicle with Curved-Wedge Forebody

Physical Insight into Fuel/Air Mixing with Hypermixer Injectors for Scramjet Engines

Applications of unstructured hybrid grid method to high-Reynolds number viscous flows

Calibration of Oxygen Atom Mass Fraction in High Enthalpy Shock Tunnel Flow Based on Shock Stand-off Distance Measurement

Numerical Study on Combustor Flow-Path Design for a Scramjet Flight Experiment

Arrangement of Rocket Engine Location in a Combined Cycle Engine

Force Measurement of Large-scale Scramjet Model within Short Test Duration

System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle

Some Aspects on Hydrocarbon-fueled RBCC Engines for a TSTO Launch Vehicle

Formation of dot arrays with a pitch of 20 nm × 20 nm for patterned media using 30 keV EB drawing on thin calixarene resist

Formation of dot arrays with a pitch of 20nm X 20nm for patterned media using 30keV EB drawing on thin calixarene resist

Free-Flight Testing in the Gas-Driven Two-Stage Light Gas Gun HEK-G

Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method

Simulation of 3D Shock Wave/Turbulent Boundary Layer Interactions by Hybrid Grid Method

Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method

Airframe- Configuration Effect on Condition of Airflow to Engine in Hypersonic Flow

衝撃波離脱距離計測による高温衝撃風洞流れの酸素原子の検定

214 Numerical Analysis of an Ethanol Fueled RBCC Engine

Force Measurement of Large-scale Scramjet Model within Short Test Duration

Considerations on Mixing and Combustion of a Scramjet Engine

Considerations on Mixing and Combustion of a Scramjet Engine. Transition Processes from Weak to Intensive Combustion Mode

Evaluation of Scramjet Testing Technology in the High Enthalpy Shock Tunnel HIEST

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