著書論文等- 永井 大樹 -
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件数:683件
[2014]
221.[] 火星探査航空機実現のための空力課題とその現状.[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),46th-32nd, (2014), ROMBUNNO.1D12-]永井大樹
222.[] 気象情報可視化ツールの開発.[可視化情報学会誌,34(135), (2014), 16-21]新井 直樹, 浅井 圭介, 永井 大樹
10.3154/jvs.34.16
223.[] S1910203 カプセル形状模型の自由飛行計測における空力特性評価([S191-02]大気突入・減速技術(2),宇宙工学部門).[年次大会,2014(0), (2014), _S1910203--_S1910203-]石田 照歩, 永井 大樹, 丹野 英幸, 小室 智幸
10.1299/jsmemecj.2014._S1910203-
224.[] F224 逆止弁付自励振動ヒートパイプの内部流動モデル構築.[熱工学コンファレンス講演論文集,2014(0), (2014), _F224-1_-_F224-2_]大丸 拓郎, 吉田 周平, 永井 大樹, 岡本 篤, 安藤 麻紀子, 杉田 寛之
10.1299/jsmeted.2014._F224-1_
225.[] 逆止弁付自励振動ヒートパイプの内部流動モデル構築.[日本機械学会熱工学コンファレンス講演論文集(CD-ROM),2014, (2014), ROMBUNNO.F224-]大丸拓郎, 吉田周平, 永井大樹, 岡本篤, 安藤麻紀子, 杉田寛之
[2013]
226.[] Aerial-Wing-Deployment Simulation of the Folded-Wing Airplane with Individual Aerodynamic Characteristics.[Proceedings of The 2013 Asia-Pacific International Symposium on Aerospace Technology,(2013)]Fujita, K., Motoda, T. and Nagai, H.
227.[] Mission Scenario of Mars Exploration by Airplane.[Proceedings of The 2013 Asia-Pacific International Symposium on Aerospace Technology,(2013)]Nagai, H. and Oyama, A.
228.[] Flow-Coupled Multibody Dynamics Simulation for an Aerial Deployment of a Folded Wing.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),726-727]Fujita, K., Motoda, T. and Nagai, H.
229.[] Aerodynamic Influence of a Propeller Wake on NACA0012 Airfoil at Low Reynolds Number.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),650-651]Makino. F., Nagai, H.
230.[] Effect of Secondary Wick on Startup Process of Loop Heat Pipe.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),696-697]Taketani. M., Nagai, H.
231.[] Development of Phosphor-TSP for High-Temperature Distribution Measurement.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),740-741]Ishida, A., Nagai, H.
232.[] Development of High-Performance TSP by Mixing Fine Particle.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),698-699]Horagiri, T., Nagai, H.
233.[] Experimental Study on Startup Behavior considering Gravity Effect of a Miniature Loop Heat Pipe.[Proceedings of The 17th International Heat Pipe Conference,(2013)]Nagai, H., Tamamura, H., Nagano, H., Ogawa. H.
234.[] 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
235.[] 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
236.[] 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
237.[] 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.
238.[] 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.
239.[] 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.
240.[] Non-Condensable Gas effect in Oscillating Heat Pipe.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
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