Nobuhiro Yamanishi

发表

An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Risk Mitigation Study of Turbine Blade Break off -

Nobuhiro Yamanishi, Hideyo Negishi, Akihide Kurosu, 2011 .

Multi Objective Shape Optimization of a Low Specific Speed Impeller for a Rocket Engine Turbopump

Nobuhiro Yamanishi, Naoki Tani, Noriyuki Shimiya, 2010 .

DEVELOPMENT AND VALIDATION OF NEW CRYOGENIC CAVITATION MODEL FOR ROCKET TURBOPUMP INDUCER

Nobuhiro Yamanishi, Shinichi Tsuda, Yoshiki Yoshida, 2009 .

Feasibility Study of Multi Objective Shape Optimization for Rocket Engine Turbopump Blade Design

Nobuhiro Yamanishi, Akira Oyama, Koichi Okita, 2008 .

Combustion and Heat Transfer Modeling in Regeneratively Cooled Thrust Chambers (Multi-Injection Flow Features)

Nobuhiro Yamanishi, Hideyo Negishi, Masaki Sasaki, 2011 .

Feasibility Study of Multi-objective Optimization of Subsystem Redundancy for Human-rated Launch Vehicle

Nobuhiro Yamanishi, Kaname Kawatsu, Koichi Okita, 2012 .

An End-to-End HighFidelity Numerical Simulation of the LE-X Engine - Combustion Chamber Risk Evaluation -

Nobuhiro Yamanishi, Akihide Kurosu, Naoki Tani, 2012 .

LE-X -Japanese Next Liquid Booster Engine-

Nobuhiro Yamanishi, Hideo Sunakawa, Akihide Kurosu, 2008 .

An Improvement of a Cavitation Model and the Application to LES

Chisachi Kato, Nobuhiro Yamanishi, Shin-ichi Tsuda, 2008 .

Combustion and Heat Transfer Modeling in Regeneratively Cooled Thrust Chambers (Co-axial Injector Flow Analysis)

Nobuhiro Yamanishi, Hideyo Negishi, Yu Daimon, 2009 .

An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Engine Performance Evaluation and Risk Mitigation Study -

Nobuhiro Yamanishi, Hideyo Negishi, Akihide Kurosu, 2011 .

Numerical Study on Rotor-Stator Interaction of a Supersonic Reaction Turbine for a Liquid Rocket Engine

Nobuhiro Yamanishi, Kaname Kawatsu, Naoki Tani, 2010 .

Transient Analysis of the LE-7A Rocket Engine Using the Rocket Engine Dynamic Simulator (REDS)

Nobuhiro Yamanishi, Hideyo Negishi, Koichi Okita, 2004 .

Large Eddy Simulation of Unsteady Flow in the LE-7A Liquid Hydrogen Pump

Nobuhiro Yamanishi, Koichi Okita, Chisachi Kato, 2007 .

504 Research on the Cryogenic Cavitation Model for Pump Inducer of Rocket Engine

Nobuhiro Yamanishi, Shinichi Tsuda, Naoki Tani, 2008 .

CFD Study for Air Ventilation Optimization in the H-II Transfer Vehicle (HTV) Pressurized Logistic Carrier (PLC)

Nobuhiro Yamanishi, Takeshi Kamiya, Tetsuya Sakashita, 2010 .

Numerical Investigation of Supercritical Coolant Flow in Liquid Rocket Engine

Nobuhiro Yamanishi, Hideyo Negishi, Yu Daimon, 2010 .

An End-to-End High Fidelity Numerical Simulation of the LE-X Engine - Influence of Coolant Leakage on Engine Power Balance -

Nobuhiro Yamanishi, Hideyo Negishi, Hideo Sunakawa, 2013 .

Reliability and Life Time Evaluation Approach of the LE-X Engine

Nobuhiro Yamanishi, Eiichi Sato, Hideo Sunakawa, 2011 .

Les analysis of a rocket turbopump inducer in non-cavitating and cavitating flows

Nobuhiro Yamanishi, Yoichiro Matsumoto, Chisachi Kato, 2003 .

Study of Next Booster Engine LE-X in JAXA

Nobuhiro Yamanishi, Akihide Kurosu, Koichi Okita, 2006 .

J101021 Investigation on CFD methodology for turbomachinery with whirling motion

Nobuhiro Yamanishi, Naoki Tani, Masaharu Uchiumi, 2013 .

Next Booster Engine LE-X in Japan

Nobuhiro Yamanishi, Akihide Kurosu, Koichi Okita, 2007 .

Combustion and Heat Transfer Modeling in Regeneratively Cooled Thrust Chambers (Wall Heat Flux Validation)

Nobuhiro Yamanishi, Hideyo Negishi, Yu Daimon, 2010 .

Application of High Fidelity Simulation to LE-X Engine Development

Nobuhiro Yamanishi, Kaname Kawatsu, Akihide Kurosu, 2011 .

Application of CFD to LE-7A OTP Alternate Inducer Development

Chisachi Kato, Nobuhiro Yamanishi, Tsutomu Mizuno, 2007 .

Numerical Analysis of Flow-Induced Structural Vibration in the LE-7A Liquid Hydrogen Pump

Nobuhiro Yamanishi, Shinobu Yoshimura, Tomonori Yamada, 2008 .

Multi Objective Optimization of a Supersonic Axial Turbine Blade Row Shape for a Rocket Engine Turbopump

Nobuhiro Yamanishi, Kaname Kawatsu, Tsutomu Mizuno, 2011 .

Aerodynamic Prediction of NASA CRM with STAR-CCM+

Nobuhiro Yamanishi, 山西伸宏, 曽我匡統, 2017 .

Elastodynamic Analysis of Fluid-Induced Vibration in the LE-7A Liquid Hydrogen Pump

Nobuhiro Yamanishi, Tomonori Yamada, Shinobu Yoshimura, 2007 .

LES Simulation of Backflow Vortex Structure at the Inlet of an Inducer

Yoshinobu Tsujimoto, Chisachi Kato, Nobuhiro Yamanishi, 2004 .

Influence of Flow Coefficient and Flow Structure on Rotational Cavitation in Inducer

Yoshinobu Tsujimoto, Nobuhiro Yamanishi, Naoki Tani, 2012 .

High-Resolution Numerical Method for Supercritical Flows with Large Density Variations

Nobuhiro Yamanishi, Soshi Kawai, Hiroshi Terashima, 2011 .

Heat Transfer Simulations in Liquid Rocket Engine Subscale Thrust Chambers

Nobuhiro Yamanishi, Hideyo Negishi, Akihide Kurosu, 2008 .

LES simulation of backflow vortex structure at the inlet of an inducer

Yoshinobu Tsujimoto, Chisachi Kato, Nobuhiro Yamanishi, 2007 .

Flowfield and Heat Transfer Characteristics of Cooling Channel Flows in a Subscale Thrust Chamber

Nobuhiro Yamanishi, Hideyo Negishi, Yu Daimon, 2011 .

A numerical study on a temporal mixing layer under transcritical conditions

Nobuhiro Yamanishi, Susumu Teramoto, Koji Okamoto, 2013 .