著書論文等- 永井 大樹 -
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件数:694件
[2016]
121.[] 将来深宇宙探査用二相流体メカニカルポンプループのシステム検討.[宇宙科学技術連合講演会講演集(CD-ROM),60th, (2016), ROMBUNNO.2K14-]坂元健一, 大丸拓郎, 永井大樹, SUNADA Eric, BHANDARI Pradeep, FURST Benjamin, CAPPUCCI Stefano
122.[] 低レイノルズ数においてプロペラ後流の影響を受ける石井翼の空力性能.[流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム講演集(CD-ROM),48th-34th, (2016), ROMBUNNO.2A17-]倉根翔, 永井大樹
123.[] 国外における超音速&極超音速柔軟構造空力減速装置の研究開発の動向について.[日本航空宇宙学会年会講演会講演集(CD-ROM),47th, (2016), ROMBUNNO.1A2-]永井大樹
124.[] Robust aerial deployment of mars airplane with tilted folding-axis.[AIAA Atmospheric Flight Mechanics Conference, (2016)]Koji Fujita, Hiroki Nagai, Akira Oyama
http://www.scopus.com/inward/record.url?eid=84958074385&partnerID=40
125.[] Development of Japanese mars airplane.[Proceedings of the International Astronautical Congress, IAC, (2016)]Hiroki Nagai, Akira Oyama
http://www.scopus.com/inward/record.url?eid=85016490565&partnerID=40
126.[] Visualization of hypersonic boundary layer transition on elliptic cone in high enthalpy shock tunnel with temperature-sensitive paint.[54th AIAA Aerospace Sciences Meeting, (2016)]Takehiro Nagayama, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro
http://www.scopus.com/inward/record.url?eid=85007564174&partnerID=40
127.[] Effect of yaw-tilted hinge axis on deployment robustness of mars airplane.[30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016, (2016)]Koji Fujita, Hiroki Nagai, Akira Oyama
http://www.scopus.com/inward/record.url?eid=85013684017&partnerID=40
128.[] 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
129.[] 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
130.[] 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]
131.[] 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
132.[] 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
133.[] 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
134.[] 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
135.[] 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
136.[] 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
137.[] 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
138.[] 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
139.[] 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
140.[] 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
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