Makoto Sato. Spatial arrangement of vortex-generator-type plasma actuator for separation control of airfoil flow. Physics of Fluids. 2025. 37. 1. 015181
Yuriko Shiratsuchi, Kento Kaneko, Shion Okada, Akira Oyama, Kazuhiko Yamada, Hiroto Tanaka, Makoto Sato. MICRO-SIZE MARS AIRPLANE FOR THE STEPWISE MARS LANDING EXPLORATION PROGRAM. ICAS 2024. 2024
Makoto Sato, Kenichi Takahama. Large-Eddy-Simulations on Dynamic Stall Control Using Plasma Actuators at Reynolds Number of 1.0×10^6. AIAA AVIATION FORUM AND ASCEND 2024. 2024. AIAA 2024-4103
Ryu Moriya, Yoshiki Nakaniida, Shusuke Honda, Makoto Sato, Eiji Shima. Numerical Investigation on Interaction Between Wing and Propeller Installed in Close Proximity to Both Upper and Lower Surfaces of Wing. AIAA AVIATION FORUM AND ASCEND 2024. 2024. AIAA 2024-4520
Yoshiki Nakaniida, Makoto Sato, Eiji Shima. Numerical Study on Aerodynamic Characteristics of Loop Propeller Toward Quiet eVTOL. AIAA AVIATION FORUM AND ASCEND 2024. 2024. AIAA 2024-4521
Large-eddy simulation on laminar-separation-bubble affected by swirling flow simulating propeller slipstream for low Reynolds number airfoil flow
(77th Annual Meeting of the Division of Fluid Dynamics 2024)
2022 - 日本流体力学会 2021年度日本流体力学会論文賞 Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 10^3-10^6
所属学会 (5件):
日本流体力学会
, American Physical Society
, American Institute of Aeronautics and Astronautics
, 日本機械学会
, 日本航空宇宙学会