著書論文等- 永井 大樹 -
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件数:694件
[2014]
221.[] Numerical study of wind-tunnel acoustic resonance induced by two-dimensional airfoil flow at low reynolds number.[29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, (2014)]Tomoaki Ikeda, Takashi Atobe, Yasufumi Konishi, Hiroki Nagai, Keisuke Asai
http://www.scopus.com/inward/record.url?eid=84910621939&partnerID=40
222.[] Propeller slipstream interference with wing aerodynamic characteristics of mars airplane at low reynolds number.[52nd Aerospace Sciences Meeting, (2014)]Fumiyasu Makino, Hiroki Nagai
http://www.scopus.com/inward/record.url?eid=84938327379&partnerID=40
223.[] Development of temperature-sensitive paint with high performance and responsivity for aerodynamic heating measurement.[52nd Aerospace Sciences Meeting, (2014)]Takehito Horagiri, Hiroki Nagai
http://www.scopus.com/inward/record.url?eid=84938330277&partnerID=40
224.[] 火星探査飛行機用推進装置の研究・開発.[宇宙科学技術連合講演会講演集(CD-ROM),58th, (2014), ROMBUNNO.1B02-]米澤宏一, 砂田茂, 大槻真嗣, 安養寺正之, 永井大樹, 浅井圭介, 岡本正人
225.[] 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
226.[] 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-
227.[] 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_
228.[] 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
229.[] 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
230.[] 自励振動ヒートパイプのスタートアップに関する一考察.[宇宙科学技術連合講演会講演集(CD-ROM),58th, (2014), ROMBUNNO.2E01-]大丸拓郎, 吉田周平, 永井大樹, 岡本篤, 安藤麻紀子, 杉田寛之
231.[] 自励振動ヒートパイプの振動形態に関する一考察.[混相流シンポジウム講演論文集(CD-ROM),2014, (2014), ROMBUNNO.B111-]吉田周平, 大丸拓郎, 永井大樹
232.[] ステンレスウイックを用いたループヒートパイプの熱輸送性能評価.[日本伝熱シンポジウム講演論文集(CD-ROM),51st, (2014), ROMBUNNO.G323-]岡崎峻, 永井大樹, 長野方星, 小川博之
[2013]
233.[] 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.
234.[] Mission Scenario of Mars Exploration by Airplane.[Proceedings of The 2013 Asia-Pacific International Symposium on Aerospace Technology,(2013)]Nagai, H. and Oyama, A.
235.[] Development of High-Performance TSP by Mixing Fine Particle.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),698-699]Horagiri, T., Nagai, H.
236.[] 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.
237.[] 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.
238.[] 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.
239.[] Development of Phosphor-TSP for High-Temperature Distribution Measurement.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),740-741]Ishida, A., Nagai, H.
240.[] 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.
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