!!Research output per year
!!Research output per year
フィンガープリント
Akiko Matsuoが活動している研究トピックを掘り下げます。このトピックラベルは、この研究者の研究成果に基づきます。これらがまとまってユニークなフィンガープリントを構成します。
- 1 類似のプロファイル
過去5年の共同研究と上位研究分野
国/地域レベルにおける最近の外部共同研究。点をクリックして詳細を開くか、または
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Design Analyses and Demonstration Tests of High-Mach Integrated Control Experiment Aircraft (HIMICO)
Taguchi, H., Sato, T., Tezuka, A., Fujio, C., Tsue, M., Tsuchiya, T., Nakaya, S., Takizawa, K., Matsuo, A., Hirotani, T., Takahashi, H., Hongoh, M., Koga, M. & Isono, T., 2026, 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. American Institute of Aeronautics and Astronautics, (27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference).研究成果: Conference contribution
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Internal Flow Structure in Rotating Detonation Engines with Non-Constant-Area Channels
Nakata, K., Kimura, T., Itouyama, N., Matsuoka, K., Kasahara, J., Kawasaki, A., Watanabe, H., Matsuo, A., Funaki, I., Higashino, K., Athmanathan, V., Meyer, T. & Paniagua, G., 2026 4月, In: AIAA journal. 64, 4, p. 2053-2064 12 p.研究成果: Article › 査読
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Numerical Evaluation of the Thermal Response of HIMICO with a Cork-Sandwich TPS
Kashiwakura, K., Matsuo, A., Shima, E., Taguchi, H., Takahashi, H. & Momose, M., 2026, 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. American Institute of Aeronautics and Astronautics, (27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference).研究成果: Conference contribution
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Operating Characteristics of Rotating Detonation Engine with Different Liquid Fuel for Next Sounding Rocket Space Flight
Matsushita, T., Sato, T., Suzuki, S., Matsuoka, K., Itouyama, N., Yasui, M., Ide, Y., Kasahara, J., Kawasaki, A., Nakata, D., Eguchi, H., Uchiumi, M., Matsuo, A. & Funaki, I., 2026, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026).研究成果: Conference contribution
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Space Flight of Liquid Rotating Detonation Engine Using Sounding Rocket S-520-34
Sato, T., Matsuoka, K., Itouyama, N., Yasui, M., Matsuyama, K., Ide, Y., Nakata, K., Suzuki, Y., Ishibashi, R., Suzuki, S., Kasahara, J., Kawasaki, A., Hirashima, H., Nakata, D., Eguchi, H., Takano, T., Uchiumi, M., Himeno, T., Yahata, Y. & Matsuo, A. & 10 others, , 2026 3月 1, In: Journal of Spacecraft and Rockets. 63, 2, p. 579-596 18 p.研究成果: Article › 査読
3 リンクは新しいタブで開きます 被引用数 (Scopus)