Aerodynamic instability of an inflatable aeroshell in suborbital re-entry von Takahashi, Yusuke, Ohashi, Tatsushi, Oshima, Nobuyuki, Nagata, Yasunori, Yamada, Kazuhiko

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Passive deployment demonstration of shape memory alloy-type deployable aeroshell using a hypersonic wind tunnel von Yamada, Kazuhiko, Akiyama, Fuya, Nagata, Yasunori

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Landing Point Analysis and Forecast Wind Data Validation for Low-Ballistic-Coefficient Flight Vehicles with a Deployable Aeroshell von NAGATA, Yasunori, YAMADA, Kazuhiko, NAKAO, Tatsuro

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Dynamic instability modeling on phase plane for thin aeroshell capsule with pitching motion at transonic speed von TAKASAWA, Hideto, FUJII, Tomoya, HIRATA, Koshiro, MORIYOSHI, Takahiro, TAKAHASHI, Yusuke, NAGATA, Yasunori, YAMADA, Kazuhiko

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Suborbital Reentry Demonstration of Inflatable Flare-Type Thin-Membrane Aeroshell Using a Sounding Rocket von Yamada, Kazuhiko, Nagata, Yasunori, Abe, Takashi, Suzuki, Kojiro, Imamura, Osamu, Akita, Daisuke

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Overall Achievements of the Flight Demonstration of EGG: Re-entry Nano-Satellite with Gossamer Aeroshell and GPS/Iridium von YAMADA, Kazuhiko, MORIYOSHI, Takahiro, MATSUMARU, Kazushige, KANEMARU, Hiroki, ARAYA, Takahiro, SUZUKI, Kojiro, IMAMURA, Osamu, AKITA, Daisuke, NAGATA, Yasunori, WATANABE, Yasumasa

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Effect of Torsion on the Friction Factor of Helical Pipe Flow von Datta, Anup Kumer, Yanase, Shinichiro, Hayamizu, Yasutaka, Kouchi, Toshinori, Nagata, Yasunori, Yamamoto, Kyoji

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Effect of new drywell cooler application for venting start time during severe accidents von ISHIDA, Naoyuki, NAGATA, Yasunori, KIMURA, Ryusuke, ANDO, Koji

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Treatment of localized prostate cancer using high‐intensity focused ultrasound von UCHIDA, TOYOAKI, OHKUSA, HIROSHI, NAGATA, YASUNORI, HYODO, TORU, SATOH, TAKEFUMI, IRIE, AKIRA

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Numerical Study of the Lift Force, Velocities and Pressure Distribution of a Single Air Bubble and Two Interacting Air Bubbles Rising in Quiescent Liquid von Guan, Chao, Yanase, Shinichiro, Matsuura, Koji, Kouchi, Toshinori, Nagata, Yasunori

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Passive deployment demonstration of shape memory alloy-type deployable aeroshell using a hypersonic wind tunnel von Yamada, Kazuhiko, Akiyama, Fuya, Nagata, Yasunori

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Mitigation of reentry blackout via gas injection in arc-heating facility von Miyashita, Takashi, Sugihara, Yuji, Takahashi, Yusuke, Nagata, Yasunori, Kihara, Hisashi

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OpenFOAM analysis of air-entraining and submerged vortices in pump sump von YAMASAKI, Ryo, KOUCHI, Toshinori, NAGATA, Yasunori, YANASE, Shinichiro

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Large-scale vortical structure detection using microphone array in a semiconductor single wafer spin cleaner von KOUCHI, Toshinori, MIYOSHI, Yuki, NAKANO, Yusuke, NAGATA, Yasunori, YANASE, Shinichiro

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Feasibility assessment of passive stabilisation for a nanosatellite with aeroshell deployed by orbit-attitude-aerodynamics simulation platform von Berthet, Maximilien, Yamada, Kazuhiko, Nagata, Yasunori, Suzuki, Kojiro

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Reentry Terminal Guidance Operation of Hayabusa2 von TSUDA, Yuichi, KIKUCHI, Shota, SAIKI, Takanao, TAKEUCHI, Hiroshi, YAMADA, Tetsuya, NAGATA, Yasunori, NAKAZAWA, Satoru, MATSUOKA, Masatoshi

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Static attitude stability of deep space sample return capsule with thin aeroshell von Takasawa, Hideto, Fujii, Tomoya, Takahashi, Yusuke, Moriyoshi, Takahiro, Takayanagi, Hiroki, Nagata, Yasunori, Yamada, Kazuhiko

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Dynamic instability modeling on phase plane for thin aeroshell capsule with pitching motion at transonic speed von TAKASAWA, Hideto, FUJII, Tomoya, HIRATA, Koshiro, MORIYOSHI, Takahiro, TAKAHASHI, Yusuke, NAGATA, Yasunori, YAMADA, Kazuhiko

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Existence of dual solutions and three-dimensional instability in helical pipe flow von Datta, Anup Kumer, Kouchi, Toshinori, Hayamizu, Yasutaka, Nagata, Yasunori, Yamamoto, Kyoji, Yanase, Shinichiro

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Numerical Study of Turbulent Helical Pipe Flow With Comparison to the Experimental Results von Datta, Anup Kumer, Hayamizu, Yasutaka, Kouchi, Toshinori, Nagata, Yasunori, Yamamoto, Kyoji, Yanase, Shinichiro

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