Kubo, N.; Bhandari, S.; Tanaka, M.; Nonomura, T.; Kawabata, H.
Experimental Parametric Study on Flow Separation Control Mechanisms around NACA0015 Airfoil Using a Plasma Actuator with Burst Actuation over Reynolds Numbers of 105–106. Appl. Sci. 2024, 14, 4652.
https://doi.org/10.3390/app14114652
AMA Style
Kubo N, Bhandari S, Tanaka M, Nonomura T, Kawabata H.
Experimental Parametric Study on Flow Separation Control Mechanisms around NACA0015 Airfoil Using a Plasma Actuator with Burst Actuation over Reynolds Numbers of 105–106. Applied Sciences. 2024; 14(11):4652.
https://doi.org/10.3390/app14114652
Chicago/Turabian Style
Kubo, Noritsugu, Sagar Bhandari, Motofumi Tanaka, Taku Nonomura, and Hirokazu Kawabata.
2024. "Experimental Parametric Study on Flow Separation Control Mechanisms around NACA0015 Airfoil Using a Plasma Actuator with Burst Actuation over Reynolds Numbers of 105–106" Applied Sciences 14, no. 11: 4652.
https://doi.org/10.3390/app14114652
APA Style
Kubo, N., Bhandari, S., Tanaka, M., Nonomura, T., & Kawabata, H.
(2024). Experimental Parametric Study on Flow Separation Control Mechanisms around NACA0015 Airfoil Using a Plasma Actuator with Burst Actuation over Reynolds Numbers of 105–106. Applied Sciences, 14(11), 4652.
https://doi.org/10.3390/app14114652