Search Results - "Anyoji, Masayuki"

Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity by Anyoji, Masayuki, Akagi, Fujio, Matsuda, Yu, Egami, Yasuhiro, Handa, Taro

“…The detailed mechanism of supersonic mixing enhancement by a novel device is investigated computationally based on the Navier-Stokes equations. The device is a…”
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First lift-off and flight performance of a tailless flapping-wing aerial robot in high-altitude environments by Tsuchiya, Shu, Aono, Hikaru, Asai, Keisuke, Nonomura, Taku, Ozawa, Yuta, Anyoji, Masayuki, Ando, Noriyasu, Kang, Chang-kwon, Pohly, Jeremy

“…Flapping flight of animals has captured the interest of researchers due to their impressive flight capabilities across diverse environments including…”
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Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number by Sekimoto, Satoshi, Fujii, Kozo, Anyoji, Masayuki, Miyakawa, Yuma, Ito, Shinichiro, Shimomura, Satoshi, Nishida, Hiroyuki, Nonomura, Taku, Matsuno, Takashi

“…In this study, an experimental investigation of separation control using a dielectric barrier discharge plasma actuator was performed on an NACA0015 airfoil…”
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Effect of Boundary Layer Trip on Reduction of Jet Noise in Over-Expanded Nozzle Flow by Anyoji, Masayuki, Tabaru, Issei

“…A flow resonance accompanied by the emission of acoustic tones occurs in an over-expanded convergent-divergent（C-D） nozzle when operated at comparatively low…”
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Design of Electrohydrodynamic Devices with Consideration of Electrostatic Energy by Sato, Tasuku, Sakuma, Shinya, Hijikuro, Masato, Maeda, Shingo, Anyoji, Masayuki, Yamanishi, Yoko

“…The importance of actuators that can be integrated with flexible robot structures and mechanisms has increased in recent years with the advance of soft…”
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Control surface effectiveness of low Reynolds number flight vehicles by Masayuki ANYOJI, Masato OKAMOTO, Hidenori HIDAKA, Katsutoshi KONDO, Akira OYAMA, Hiroki NAGAI, Kozo FUJII

“…Low-speed wind tunnel tests are carried out to investigate the control surface effectiveness at low Reynolds numbers (Re = 20,000-80,000). A thick airfoil,…”
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Deflector effect on flow behavior and drag of an Ahmed body under crosswind conditions by The Hung, Tran, Hijikuro, Masato, Anyoji, Masayuki, Uchida, Takanori, Nakashima, Takuji, Shimizu, Keigo

“…This study investigates the effect of a deflector on Ahmed model drag and the flow on the slant during steady crosswind conditions by experimental methods at a…”
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Surface flow and aerodynamic drag of Ahmed body with deflectors by Hung Tran, The, Hijikuro, Masato, Anyoji, Masayuki, Uchida, Takanori, Nakashima, Takuji, Shimizu, Keigo

“…•Flow on the slant surface, force and pressure are analyzed for Ahmed body with deflectors.•At the deflection angle above −5°, total drag, flow fields, and…”
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Analysis of nozzle geometry effect on supersonic jet noise using Schlieren by Ozawa, Yuta, Oyama, Akira, Anyoji, Masayuki, Mamori, Hiroya, Fukushima, Naoya, Yamamoto, Makoto, Fujii, Kozo

“…Strong acoustic waves emitted from rocket plume might damage to rocket payloads because rocket payloads consist of fragile structure. Therefore, it is…”
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Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel by Anyoji, M., Numata, D., Nagai, H., Asai, K.

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