著書論文等- 永井 大樹 -
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件数:705件
[2014]
241.[] 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
242.[] 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
243.[] Development of temperature-sensitive paint with high performance and responsivity for aerodynamic heating measurement.[52nd Aerospace Sciences Meeting, (2014)]Takehito Horagiri, Hiroki Nagai
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[2013]
244.[] 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.
245.[] Mission Scenario of Mars Exploration by Airplane.[Proceedings of The 2013 Asia-Pacific International Symposium on Aerospace Technology,(2013)]Nagai, H. and Oyama, A.
246.[] Development of High-Performance TSP by Mixing Fine Particle.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),698-699]Horagiri, T., Nagai, H.
247.[] 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.
248.[] 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.
249.[] 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.
250.[] Development of Phosphor-TSP for High-Temperature Distribution Measurement.[Proceedings of 10th International Conference on Fluid Dynamics,(2013),740-741]Ishida, A., Nagai, H.
251.[] 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.
252.[] 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
253.[] 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
254.[] 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
255.[] 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.
256.[] 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.
257.[] 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.
258.[] Non-Condensable Gas effect in Oscillating Heat Pipe.[Proceedings of 43rd International Conference on Environmental Systems,(2013)]Daimaru, T. and Nagai, H.
259.[] 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
260.[] 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.
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