Masahiro Kanazaki

发表

Robust Constrained Multi-objective Evolutionary Algorithm based on Polynomial Chaos Expansion for Trajectory Optimization

Yuji Takubo, Masahiro Kanazaki, 2022, 2022 IEEE Congress on Evolutionary Computation (CEC).

Numerical investigation of wake structures of an atmospheric entry capsule by modal analysis

Y. Ohmichi, K. Kobayashi, Masahiro Kanazaki, 2019, Physics of Fluids.

Numerical Study of Coherent Structures Around a Re-entry Capsule using Proper Orthogonal Decomposition

Y. Ohmichi, Keiichi Ishiko, Masahiro Kanazaki, 2017 .

Implication of Fuels in Performance of Single-stage Launch Vehicle with Hybrid Rocket Engine

Masahiro Kanazaki, Kazuhisa Chiba, Koki Kitagawa, 2013, International Conference on Simulation and Modeling Methodologies, Technologies and Applications.

Design Methodology of a Hybrid Rocket-Powered Launch Vehicle for Suborbital Flight

Masahiro Kanazaki, Kazuhisa Chiba, Koki Kitagawa, 2017 .

Multi-Objective Aerodynamic Optimization of Elements' Setting for High-lift Airfoil Using Kriging Model

Kazuomi Yamamoto, Masahiro Kanazaki, Shinkyu Jeong, 2006 .

Multi-Fidelity Multi-Objective Efficient Global Optimization Applied to Airfoil Design Problems

Masahiro Kanazaki, Atthaphon Ariyarit, Atthaphon Ariyarit, 2017 .

DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION

M. Kanazaki, Y. Tanabe, Atthaphon Ariyarit, 2016 .

Numerical Analysis on Hovering Performance of Hexacopter “HAMILTON” for Mars Exploration

A. Oyama, Y. Tanabe, M. Sugiura, 2022, AIAA AVIATION 2022 Forum.

Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing

Kazuomi Yamamoto, Masahiro Kanazaki, Mitsuhiro Murayama, 2008 .

Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design

Masahiro Kanazaki, Masahiko Sugiura, Yasutada Tanabe, 2017 .

Multi-Objective Design Optimization System for a Subsonic Diffuser

Masahiro Kanazaki, Masahiro Kanazaki, 2004 .

Exhaust manifold design with tapered pipes using divided range MOGA

Kazuhiro Nakahashi, Shigeru Obayashi, Masahiro Kanazaki, 2004 .

EXHAUST MANIFOLD DESIGN FOR A CAR ENGINE BASED ON ENGINE CYCLE SIMULATION

Kazuhiro Nakahashi, Shigeru Obayashi, Masahiro Kanazaki, 2003 .

Multiobjective Design Optimization of Merging Configuration for an Exhaust Manifold of a Car Engine

Kazuhiro Nakahashi, Shigeru Obayashi, Masahiro Kanazaki, 2002, PPSN.

Mixed-fidelity Efficient Global Optimization Applied to Design of Supersonic Wing

H. Takagi, Y. Makino, M. Kanazaki, 2013 .

Design exploration of high-lift airfoil using Kriging model and data mining technique

Masahiro Kanazaki, Shinkyu Jeong, K. Tanaka, 2006 .

Influence of Pre-twist Distribution at the Rotor Blade Tip on Performance during Hovering Flight

Masahiko Sugiura, Yasutada Tanabe, Masatoshi Harigae, 2015 .

Nacelle Chine Installation Based on Wind-Tunnel Test Using Efficient Global Optimization

Kazuomi Yamamoto, Mitsuhiro Murayama, Takeshi Ito, 2008 .

High-Lift System Optimization Based on the Kriging Model Using a High-Fidelity Flow Solver

Kazuomi Yamamoto, Masahiro Kanazaki, Shinkyu Jeong, 2006 .

Hypothesis derivation and its verification by a wholly automated many-objective evolutionary optimization system

Masahiro Kanazaki, Kazuhisa Chiba, Taiki Hatta, 2021, Neural Computing and Applications.

Effective operations of hybrid-rocket extinction-reignition via oxidizer-mass-flow control

千葉一永, 金崎雅博, Masahiro Kanazaki, 2016 .

Ascendancy of extinction-reignition on single-stage hybrid sounding rocket in view of fuels

Shinya Watanabe, Masahiro Kanazaki, Kazuhisa Chiba, 2016 .

MANIFESTATION OF ASCENDANCY OF EXTINCTION-REIGNITION ON SOUNDING HYBRID ROCKET USING DESIGN INFORMATICS

Masahiro Kanazaki, Kazuhisa Chiba, Toru Shimada, 2016 .

Visualization of Design-Space Constitution for Single-Stage Hybrid Rocket with Rigid Body in View of Extinction-Reignition

Masahiro Kanazaki, Kazuhisa Chiba, Hideyuki Yoda, 2015, 2015 IEEE Symposium Series on Computational Intelligence.

Multidisciplinary Design Exploration for Sounding Launch Vehicle using Hybrid Rocket Engine in View of Ballistic Performance

Masahiro Kanazaki, Kazuhisa Chiba, Koki Kitagawa, 2015 .

NUMERICAL SIMULATION OF SUPERSONIC INTAKE USING STRUCTURED-UNSTRUCTURED ZONAL APPROACH

S. Obayashi, K. Nakahashi, Yasushi Ito, 2004 .

Multi-Objective Aerodynamic Exploration of Elements’ Setting for High-Lift Airfoil Using Kriging Model

Kazuomi Yamamoto, Shinkyu Jeong, Masahiro Kanazaki, 2006 .

Wing planform dependency on optimum supersonic airfoil

Masahiro Kanazaki, Kisa Matsushima, Yuki Kishi, 2017 .

Influence of Engine Intake/Exhaust on Wing Design of Civil Aircraft by Means of Knowledge Discovery Techniques

Kazuomi Yamamoto, Mitsuhiro Murayama, Masahiro Kanazaki, 2016 .

1305 Aerodynamic Design Optimization of Low Noise High-Lift Airfoil for Civil Aircraft

Kazuomi Yamamoto, Mitsuhiro Murayama, Masahiro Kanazaki, 2013 .

CFD analysis on sweep angles of the leading and trailing edges of a wing in a supersonic flow

Kazuhiro Kusunose, Masahiro Kanazaki, Kisa Matsushima, 2015 .

Hybrid Method of Prescribed Wake Model and CFD for Helicopter BVI Noise Prediction by

Y. Tanabe, M. Sugiura, S. Saito, 2013 .

Hybrid method of CFD and prescribed wake model for rotorcraft aeroacoustics and aerodynamics prediction

Masahiro Kanazaki, Masahiko Sugiura, Yasutada Tanabe, 2012 .

Experiment and computation multi-fidelity multi-objective airfoil design optimization of fixed-wing UAV

Masahiro Kanazaki, Atthaphon Ariyarit, Yuki Kishi, 2021, Journal of Mechanical Science and Technology.

Numerical Simulation of Supersonic Flow around Wing-Body Configuration with Integrated Engine Nacelle

Kazuhiro Nakahashi, Shigeru Obayashi, Masahiro Kanazaki, 2002 .

Blade Element Theory Coupled with CFD Applied to Optimal Design of Rotor for Mars Exploration Helicopter

A. Oyama, H. Nagai, Koji Fujita, 2020 .

Modal Decomposition Analysis of Subsonic Unsteady Flow Around An Atmospheric Entry Capsule with Forced Oscillation

Kenji Kobayashi, Y. Ohmichi, M. Kanazaki, 2019, AIAA Scitech 2019 Forum.

Evolutionary Multidisciplinary Design Optimization of Blended-Wing-Body-Type Flyback Booster

Naoki Hamada, Masahiro Kanazaki, Koichi Yonemoto, 2019, AIAA Scitech 2019 Forum.

Trajectory and Aerodynamic Control Optimization of Civil Aircraft Descent Under Hazard Situations Based on High-Fidelity Aerodynamic Database

Masahiro Kanazaki, Norazila Othman, N. Othman, 2016 .

Design Exploration of Airfoil Geometry for Martian Airplane

Masahiro Kanazaki, Masahiro Kanazaki, 2015 .

Multi-segment Class-Shape-Transformation (CST) for global design exploration

M. Kanazaki, Atthaphon Ariyarit, Masahiro Kanazaki, 2014, 2014 10th France-Japan/ 8th Europe-Asia Congress on Mecatronics (MECATRONICS2014- Tokyo).

Unsteady Numerical Simulations of HTV-R Reentry Capsule by Using Detached-Eddy Simulation

T. Aoyama, A. Hashimoto, M. Kanazaki, 2014 .

Parametric Airfoil Representation toward Efficient Design Knowledge Discovery under Various Flow Condition

Masahiro Kanazaki, Takaya Sato, Kisa Matsushima, 2014 .

Challenge of design exploration for small blended wing body using unstructured flow solver

Kazuomi Yamamoto, Mitsuhiro Murayama, Masahiro Kanazaki, 2013 .

Numerical Simulation of Supersonic Flow around Wing-Body Configuration with Integrated Engine Nacelle

Kazuhiro Nakahashi, Shigeru Obayashi, Masahiro Kanazaki, 2002 .

Application of Simulation Design Optimization Techniques in Aerospace Engineering

Masahiro Kanazaki, Masahiro Kanazaki, 2013 .

Numerical Simulation of Supersonic Flow around Wing-Body Configuration with Integrated Engine Nacelle

Kazuhiro Nakahashi, Shigeru Obayashi, Masahiro Kanazaki, 2002 .

Planform dependency of optimum cross-sectional geometric distributions for supersonic wing

Y. Makino, M. Kanazaki, Atthaphon Ariyarit, 2019, Aerospace Science and Technology.

Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic

Masahiro Kanazaki, Kisa Matsushima, Yoshikazu Makino, 2016 .

Efficient Design Exploration of Nacelle Chine Installation in Wind Tunnel Testing

Mitsuhiro Murayama, Kazuomi Yamamoto, Takeshi Ito, 2008 .

1802 High-lift Airfoil Design for a Take-Off Configuration Using Kriging Based GA

Kazuomi Yamamoto, Mitsuhiro Murayama, Masahiro Kanazaki, 2007 .

Hybrid Propulsion Technology Development in Japan for Economic Space Launch

Harunori Nagata, Keiichi Hori, Keisuke Sawada, 2017 .

Conceptual Helicopter Design for Exploration of Pit craters and Caves on Mars

A. Oyama, H. Nagai, Koji Fujita, 2018, 2018 AIAA SPACE and Astronautics Forum and Exposition.

An Approach Combining an Efficient and Global Evolutionary Algorithm with a Gradient-Based Method for Airfoil Design Problems

Sujin Bureerat, Masahiro Kanazaki, Atthaphon Ariyarit, 2020, Smart Science.

Hybrid Rocket Engine Design Using Pairwise Ranking Surrogate-assisted Differential Evolution

Tomohiro Harada, Masahiro Kanazaki, Y. Miura, 2023, GECCO Companion.

Evolutionary algorithm applied to time-series landing flight path and control optimization of supersonic transport

Masahiro Kanazaki, Ryouta Saisyo, Nao Setoguchi, 2021, Neural Computing and Applications.

Genetic Algorithm Applied to the Time-Series Landing Flight Path and Control Optimization of a Supersonic Transport

Masahiro Kanazaki, Ryouta Saisyo, Masahiro Kanazaki, 2019, Proceedings of the 2019 3rd International Conference on Intelligent Systems, Metaheuristics & Swarm Intelligence.

Genetic Algorithm Applied to Design Knowledge Discovery of Launch Vehicle Using Clustered Hybrid Rocket

Masahiro Kanazaki, Kazuhisa Chiba, Koki Kitagawa, 2018, Computational Methods in Applied Sciences.

Evolutionary algorithm applied to ballistic launch vehicle design using hybrid rocket engine evaluated by enhanced flight simulation

Masahiro Kanazaki, Kazuhisa Chiba, Koki Kitagawa, 2015, 2015 IEEE Congress on Evolutionary Computation (CEC).

Multi-modal distribution crossover method based on two crossing segments bounded by selected parents applied to multi-objective design optimization

Masahiro Kanazaki, Atthaphon Ariyarit, M. Kanazaki, 2015 .

Multi-modal distribution crossover method based on two crossing segments bounded by selected parents applied to multi-objective design optimization

Atthaphon Ariyarit, Masahiro Kanazaki, 2015, Journal of Mechanical Science and Technology.

Improvement of Flow Control Performance of Plasma Actuator Using Wind-Tunnel Test Based Efficient Global Optimization

Takashi Matsuno, Gouji Yamada, Masahiro Kanazaki, 2013 .

Design optimization of launch vehicle concept using cluster hybrid rocket engine for future space transportation

Masahiro Kanazaki, Fumio Kanamori, Masaki Nakamiya, 2016 .

Preface

Masahiro Kanazaki, Kazuhisa Chiba, 2022, Journal of the Visualization Society of Japan.

Simple control of oxidizer flux for efficient extinction–reignition on a single-stage hybrid rocket

Kazuhisa Chiba, Toru Shimada, Masahiro Kanazaki, 2017 .

Low-Boom Design for Supersonic Transport with Canard and Forward-Swept Wings Using Equivalent Area Design Method

Yuki Kishi, Masahiro Kanazaki, Risato Yashiro, 2023, Aerospace.

Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization

Y. Makino, Yuki Kishi, Masahiro Kanazaki, 2022, Journal of Aircraft.

Numerical Investigation of Sonic Boom for Forward-Swept Wing Based on Euler and Augmented Burgers Equations

Y. Makino, Yuki Kishi, Masahiro Kanazaki, 2020 .

Development of Digital Flight Motion Methodology Based on Aerodynamic Derivatives Approximation

Masahiro Kanazaki, Norazila Binti Othman, N. Othman, 2016, J. Robotics Mechatronics.

Efficient Flight Simulation Using Kriging Surrogate Model Based Aerodynamic Database

Masahiro Kanazaki, Norazila Othman, N. Othman, 2015 .