Kozo Fujii

University of Tokyo

Japan

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Articles (10)

Comparison of Separation Control Mechanisms for Synthetic Jet and Plasma Actuators

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Year:

2023

Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number

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Year:

2023

Flow instability and momentum exchange in separation control by a synthetic jet

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Year:

2023

Rule Design for Interpretable En Route Arrival Management via Runway-Flow and Inter-Aircraft Control

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Year:

2023

Computational Study of the Plasma Actuator Flow Control for an Airfoil at Pre-Stall Angles of Attack

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Year:

2022

Sound source characteristics generated by shocklets in isotropic compressible turbulence

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Year:

2022

In-Flight Demonstration of Stall Improvement Using a Plasma Actuator for a Small Unmanned Aerial Vehicle

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Year:

2022

Computational study on aeroacoustic fields of a transitional supersonic jet

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Year:

2021

Dynamic Burst Actuation to Enhance the Flow Control Authority of Plasma Actuators

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Year:

2021

Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder

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Year:

2021

Collaborators (3)

Taku Nonomura

Associate Professor

Tohoku University

JAPAN

Hikaru Aono

associate professor

Shinshu Daigaku - Ueda Campus

JAPAN

Yuta Ozawa

Project Assistant Professor

Tohoku Daigaku

JAPAN

Kozo Fujii

Research Interests

Explore related searches

Contact this professor

Articles (10)

Comparison of Separation Control Mechanisms for Synthetic Jet and Plasma Actuators

Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number

Flow instability and momentum exchange in separation control by a synthetic jet

Rule Design for Interpretable En Route Arrival Management via Runway-Flow and Inter-Aircraft Control

Computational Study of the Plasma Actuator Flow Control for an Airfoil at Pre-Stall Angles of Attack

Sound source characteristics generated by shocklets in isotropic compressible turbulence

In-Flight Demonstration of Stall Improvement Using a Plasma Actuator for a Small Unmanned Aerial Vehicle

Computational study on aeroacoustic fields of a transitional supersonic jet

Dynamic Burst Actuation to Enhance the Flow Control Authority of Plasma Actuators

Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder

Collaborators (3)

Taku Nonomura

Hikaru Aono

Yuta Ozawa

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