Acquisition of Swept Aerodynamic Data by the Consecutive Changing of Wing Model Configuration in a Wind Tunnel Test Using Remote Feedback Control by Ken Wakimoto, Kazuhisa Chiba, Hiroyuki Kato, Kazuyuki Nakakita

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Remote and Feedback Control of the Flap Angle in a Wind Tunnel Test Model by Optical Measurement by Kazuhisa Chiba, Tatsuro Komatsu, Hiroyuki Kato, Kazuyuki Nakakita

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Structural and Aeroelastic Studies of Wing Model with Metal Additive Manufacturing for Transonic Wind Tunnel Test by NACA 0008 Example by Natsuki Tsushima, Kenichi Saitoh, Hitoshi Arizono, Kazuyuki Nakakita

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Optimum layout of vortex generators for upper surface of wing using efficient global optimization by Norikazu KOZAKAI, Hiroyuki KATO, Kazuyuki NAKAKITA, Masahiro KANAZAKI

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Investigation of Factors Causing Nonuniformity in Luminescence Lifetime of Fast-Responding Pressure-Sensitive Paints by Yasuhiro Egami, Yuya Yamazaki, Naoto Hori, Yosuke Sugioka, Kazuyuki Nakakita

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Reduction in Airfoil Trailing-Edge Noise Using a Pulsed Laser as an Actuator by Keita Ogura, Yoimi Kojima, Masato Imai, Kohei Konishi, Kazuyuki Nakakita, Masaharu Kameda

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Evaluation of the Characteristics and Coating Film Structure of Polymer/Ceramic Pressure-Sensitive Paint by Yosuke Sugioka, Kazuto Arakida, Miku Kasai, Taku Nonomura, Keisuke Asai, Yasuhiro Egami, Kazuyuki Nakakita

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Dynamic Stall Control around Practical Airfoil Using Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators by Yuto Iwasaki, Taku Nonomura, Koki Nankai, Keisuke Asai, Shoki Kanno, Kento Suzuki, Atsushi Komuro, Akira Ando, Keisuke Takashima, Toshiro Kaneko, Hidemasa Yasuda, Kenji Hayama, Tomoka Tsujiuchi, Tsutomu Nakajima, Kazuyuki Nakakita

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