著書論文等- 永井 大樹 -
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件数:694件
[2013]
241.[] ループヒートパイプの熱特性におけるセカンダリウィックの影響.[宇宙科学技術連合講演会講演集,57, (2013), 6p-]竹谷 政彦, 永井 大樹
242.[] 火星大気を飛行する航空機の第一次熱設計.[宇宙科学技術連合講演会講演集,57, (2013), 6p-]大丸 拓郎, 永井 大樹
243.[] 大気球を利用した火星探査航空機の高高度飛行実証機に関する熱的検討.[宇宙科学技術連合講演会講演集,57, (2013), 5p-]永井 大樹, 大丸 拓郎
244.[] Preliminary design and thermal analysis of a miniature Mars airplane thermal control system.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
245.[] Numerical Study on Shock Wave Interaction over Compression Corner with 30 deg. in Hypersonic Flow.[Proceedings of 29th International Symposium on Shock Waves,(2013)]Kuramoto, T., Tsuboi, N. and Nagai, H., Asai, K.
246.[] Operational characteristics of the Oscillating Heat Pipe with non-condensable gas.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
247.[] Non-Condensable Gas effect in Oscillating Heat Pipe.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
248.[] 空力加熱計測のための高性能・高応答感温塗料の開発.[可視化情報学会誌,33(Suppl.1), (2013), 493‐498-]洞桐健人, 永井大樹
249.[] Numerical Simulation of Startup Behavior of Loop Heat Pipes with Secondary Wick.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Magome, K., Taketani, M., Nagai, H.
250.[] Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Makino, F., Nagai, H. and Asai, K.
251.[] Experimental Investigation of Non-condensable Gas effects on the Oscillating Heat Pipe.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Daimaru, T. and Nagai, H.
252.[] Dynamic Behaviour of Mars Airplane with Folded-Wing Deployment.[Proceedings of 29th International Symposium on Space Technology and Science,(2013)]Fujita, K., Motoda, Y. and Nagai, H.
253.[] 極超音速流れにおける30°ランプ周りの衝撃波干渉に関する数値解析:スパン幅が流れ場構造に与える影響.[衝撃波シンポジウム講演論文集,2012, (2013), 335-338]倉本健史, 武藤大貴, 坪井伸幸, 永井大樹, 浅井圭介
254.[] Characteristics of Low-Reynolds Number Airfoils in a Mars Wind Tunnel.[Proceedings of 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition,(2013)]Nagai, H., Asai, K., Numata, D., Suwa, T. and Anyoji, M.
255.[] Development of Ultrafast Response Anodized Aluminum Pressure-Sensitive Paints.[Proceedings of 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition,(2013)]Fujii, S., Numata, D., Nagai, H. and Asai, K.
256.[] 火星探査飛行機用プロペラ開発のための翼型に関する研究.[日本航空宇宙学会論文集,61,(2013),421-]米 澤 宏 一,後 藤 雄 大,砂 田 茂,林 田 高 志,諏 訪 哲 也,酒 井 宣 明,永 井 大 樹,浅 井 圭 介,辻 本 良 信
257.[] Aerodynamic Characteristics and Effects of Winglets of the Boomless Tapered Supersonic Biplane during the Starting Process.[Trans. JSASS Aerospace Tech. Japan,11,(2013),17-26]Yamashita, H., Fujisono, T., Toyoda, A., Nagai, H., Asai, K., Jeong . and Obayashi, S.
258.[] Heat Transfer Performance of Oscillating Heat Pipe by Difference of Surface Characteristics.[Proceedings of the 17th International Heat Pipe Conference,(2013)]Hiroki Nagai, Takamu Kanayama, Takurou Daimaru
259.[] Experimental Study on Startup Behavior considering Gravity Effect of a Miniature Loop Heat Pipe.[Proceedings of the 17th International Heat Pipe Conference,(2013)]Hiroki Nagai, Horomichi Tamamura, Hosei Nagano, Hiroyuki Ogawa
260.[] Preliminary design and thermal analysis of a miniature mars airplane thermal control system.[43rd International Conference on Environmental Systems, (2013)]Takurou Daimaru, Hiroki Nagai
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