著書論文等- 永井 大樹 -
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件数:683件
[2016]
121.[] Experimental Study of Effects of Secondary Wick Configuration on Thermal Performance of Loop Heat Pipe.[TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,14(30), (2016), Pi_7-Pi_15]NAGAI Hiroki, TAKETANI Masahiko, ADACHI Takuya, DAIMARU Takurou
10.2322/tastj.14.Pi_7
122.[] A Parametric Study of Mars Airplane Concept for Science Mission on Mars.[TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,14(30), (2016), Pk_83-Pk_88]FUJITA Koji, NAGAI Hiroki, OYAMA Akira
10.2322/tastj.14.Pk_83
123.[] Development of a Cooling System for GAPS using Oscillating Heat Pipe.[TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,14(30), (2016), Pi_17-Pi_26]FUKE Hideyuki, MIYAZAKI Yoshiro, MORI Junichi, NAGAI Hiroki, NONOMURA Taku, OGAWA Hiroyuki, OKAZAKI Shun, OKUBO Takuma, OZAKI Shinji, SATO Daisuke, SHIMIZU Kensei, ABE Takumi, TAKAHASHI Katsumasa, TAKAHASHI Shun, YAMADA Noboru, YOSHIDA Takanori, DAIMARU Takuro, INOUE Takayoshi, KAWACHI Akiko, KAWAI Hiroki, MASUYAMA Yosuke, MATSUMIYA Hiroaki, MATSUMOTO Daishi
10.2322/tastj.14.Pi_17
[2015]
124.[] Evaluation of Aerodynamic Characteristics of an Optimized Airfoil for Mars Airplane.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Kentarou Yamahara, Daisuke Oshiyama, Hiroki Nagai, Masahiro Kanazaki, Daiju Numata, Keisuke Asai
125.[] Development of the Makita-Type Active Turbulence Grid for 03-m Wind Tunnel.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Satoru Hatori, Hiroki Nagai, Daiju Numata, Keisuke Asai
126.[] Application of Temperature-Sensitive Paint to High-Enthalpy Shock Tunnel for Visualization of Boundary Layer Transition.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Takehito Nagayama, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro
127.[] Flow Visualization of Oscillating Heat Pipe by X-ray Imaging Method.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Shuhei Yoshida, Takurou Daimaru, Masahiro Kawaji, Hiroki Nagai
128.[] Effects of Check Valves on Thermal and Flow Characteristics of Oscillating Heat Pipes.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai
129.[] 火星飛行機の空中展開に対するヒンジ軸傾斜の効果.[宇宙科学技術連合講演会講演集,59, (2015), 6p-]藤田 昂志, 永井 大樹, 大山 聖
130.[] 自励振動ヒートパイプの動作特性における逆止弁の影響.[宇宙科学技術連合講演会講演集,59, (2015), 5p-]大丸 拓郎, 吉田 周平, 永井 大樹
131.[] 先進熱制御デバイスを用いたDESTINY熱設計.[宇宙科学技術連合講演会講演集,59, (2015), 6p-]岡崎 峻, 長野 方星, 永井 大樹
132.[] 数値解析による自励振動ヒートパイプ内の熱サイクルに関する研究.[Thermophysical Properties,36th, (2015), 69‐71-]大丸拓郎, 吉田周平, 永井大樹
133.[] 感温塗料計測技術の高温衝撃風洞HIESTへの適用.[Thermophysical Properties,36th, (2015), 63‐65-]永井大樹, 長山剛大, 丹野英幸, 小室智幸
134.[] 可視化によるチェックバルブ付き自励振動ヒートパイプの循環流に関する考察.[Thermophysical Properties,36th, (2015), 84‐86-]吉田周平, 大丸拓郎, 永井大樹, LIU Tianshu, 沼田大樹, 浅井圭介
135.[] 逆止弁付き振動流型ヒートパイプの設計最適化を目指した熱輸送特性評価.[Thermophysical Properties,36th, (2015), 66‐68-]田中洸輔, 安藤麻紀子, 岡本篤, 杉田寛之, 大丸拓郎, 永井大樹
136.[] 感温塗料を用いた高温衝撃風洞におけるHIFiRE模型の境界層遷移可視化.[日本機械学会年次大会講演論文集(CD-ROM),2015, (2015), ROMBUNNO.S1910301-]長山剛大, 永井大樹, 丹野英幸, 小室智幸
137.[] Visualization of Loop Heat Pipe with Multiple Evaporators under Microgravity.[Proceedings of the 45th International Conference on Environmental Systems,(2015)]Hosei Nagano, Yuta Matsuda, Shun Okazaki, Hiroki Nagai, Hiroyuki Ogawa
138.[] Parametric Study of Oscillating Heat Pipes by using Mathematical Model for Practical Use in Spacecraft.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando, Hiroyuki Sugita
139.[] Aerodynamic Characteristics of Airfoils with Different Aspect Ratio behind Propeller Slipstream in Low Reynolds Number Condition.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Kotaro Watanabe, Koji Fujita
140.[] Aerodynamic Challenge to Realize Mars Airplane.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Masayuki Anyoji, Taku Nonomura, Akira Oyama, Masato Okamoto, Gaku Sasaki, Takaaki Matsumoto, Kouichi Yonemoto, Kasahiro Kanazaki, Shigeru Sunada, Koichi Yonezawa, Masaru Koike, Koji Fujita, Keisuke Asai, Kozo Fujii
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