論文- 永井 大樹 -
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件数:235件
[2015]
41.Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows.[AIAA Journal,53(6),(2015),1640-1654]Masayuki Anyoji, Daiju Numata, Hiroki Nagai, Keisuke Asai
42.Pressure-Sensitive Paint Technique for Surface Pressure Measurement in a Low Density Wind Tunnel.[Journal of Visualization,18(2),(2015),297-309]Masayuki Anyoji, Daiju Numata, Hiroki Nagai, Keisuke Asai
43.マルチエバポレータ型ループヒートパイプ内部流動特性に関する研究(微小重力下での蒸発器及び凝縮器の可視化).[日本機械学会論文集,81(827),(2015),15-00104-]松田雄太,長野方星,岡崎峻,小川博之,永井大樹
1299/transjsme.15-00104, 2015
44.マルチエバポレータ型ループヒートパイプの内部流動特性に関する研究(微小重力環境下での蒸発器及び凝縮器の可視化).[日本機械学会論文集,81(827),(2015),15-00104-15-00104]松田 雄太, 長野 方星, 岡崎 峻, 小川 博之, 永井 大樹
10.1299/transjsme.15-00104
[2014]
45.Computational and experimental analysis of a high-performance airfoil under low-reynolds-number flow condition.[Journal of Aircraft,51(6),(2014),1864-1872]Masayuki Anyoji, Taku Nonomura, Hikaru Aono, Akira Oyama, Kozo Fujii, Hiroki Nagai, Keisuke Asai
10.2514/1.C032553
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000345980800015&DestApp=WOS http://www.scopus.com/inward/record.url?eid=84914171144&partnerID=40
46.Visualization of Laminar to Turbulent Transition on Re-entry Capsule using TSP in High Enthalpy Shock Tunnel.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Takehiro Nagayama, Takehito Horagiri, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro
47.Aerodynamic performance of optimized airfoil for Mars Airplane using Multi-objective generic algorithm.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Kentaro Yamahara, Hiroki Nagai, Takaya Sato and Masahiro Kanazaki
48.Effect of blade wake by means of interference with propeller slipstream on low Reynolds number condition.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Satoru Hattori, Kotaro Watanabe, Hiroki Nagai
49.Improvement of Startup Characteristics of a Loop Heat Pipe using Secondary Wicks.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Masahiko Taketani, Hiroki Nagai
50.Study of Motion Modeling for a Capsule Shaped Projectile in Free flight Testing at Transonic.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Akiho Ishida, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komoro
51.Numerical Investigation of the Effects of Initial Liquid-Vapor Distribution in Oscillating Heat Pipes.[Proceedings of the 11th International Conference on Flow Dynamics,(2014)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando, Hiroyuki Sugita
52.Numerical Study of Wind-Tunnel Acoustic Resonance induced by Two-Dimensional Airfoil Flow at Low Reynolds Number.[Proceedings of the 29th Congress of the International Council of the Aeronautical Science,(2014)]1. Tomoaki Ikeda, Takashi Atobe, Yasuhiro Konishi, Hiroki Nagai, Keisuke Asai
53.Effects of Secondary Wicks on the Thermal Performance of a Loop Heat Pipe.[Proceedings of 44rd International Conference on Environmental Systems,(2014)]Masahiko Taketani and Hiroki Nagai
54.Operation Characteristics of Loop Heat Pipes with PTEF and SUS wicks.[Proceedings of 44rd International Conference on Environmental Systems,(2014)]Shun Okazaki, Hosei Nagano, Hiroki Nagai and Hiroyuki Ogawa
55.Mathematical Modeling and Experimental Validation of Oscillating Heat Pipes.[Proceedings of 44rd International Conference on Environmental Systems,(2014)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando and Hiroyuki Sugita
56.Visualization of a Re-entry Vehicle in Hypersonic Flow using Temperature-Sensitive Paint.[Proceedings of the 16th International Symposium on Flow Visualization,(2014)]Hiroki Nagai, Takehito Horagiri, Hideyuki Tannno and Tomoyuki Komuro
57.Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing.[International Journal of Aerospace Engineering,2013,(2014)]Hiroshi Yamashita, Naoshi Kuratani, Masahito Yonezawa, Toshihiro Ogawa, Hiroki Nagai, Keisuke Asai and Shigeru Obayashi
10.1155/2013/231434
58.Propeller Slipstream Interference with Wing Aerodynamic Characteristics of Mars Airplane at Low Reynolds Number.[Trans. of JSASS Aerospace Tech. Japan,12(ists29),(2014),Tk_13-Tk_18]Making, F. and Nagai, H.
59.Dynamic Behaviour of Mars Airplane with Folded-Wing Deployment.[Trans. of JSASS Aerospace Tech. Japan,12(ists29),(2014),Pk_1-Pk_6]Fujita, K, Motoda, T. and Nagai, H.
60.Development of Temperature-Sensitive Paint with High Performance and Responsivity for Aerodynamic Heating Measurement.[Proceedings of AIAA SciTech2014,(2014)]Horagiri, T. and Nagai, H.
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