論文- 永井 大樹 -
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件数:232件
[2016]
21.Comparing Aerial-Deployment-Mechanism designs for mars airplane.[Transactions of the Japan Society for Aeronautical and Space Sciences,59(6),(2016),323-331]Koji Fujita, Hiroki Nagai
10.2322/tjsass.59.323
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000386933700002&DestApp=WOS http://www.scopus.com/inward/record.url?eid=84994553174&partnerID=40
[2015]
22.Evaluation of Aerodynamic Characteristics of an Optimized Airfoil for Mars Airplane.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Kentarou Yamahara, Daisuke Oshiyama, Hiroki Nagai, Masahiro Kanazaki, Daiju Numata, Keisuke Asai
23.Development of the Makita-Type Active Turbulence Grid for 03-m Wind Tunnel.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Satoru Hatori, Hiroki Nagai, Daiju Numata, Keisuke Asai
24.Application of Temperature-Sensitive Paint to High-Enthalpy Shock Tunnel for Visualization of Boundary Layer Transition.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Takehito Nagayama, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komuro
25.Flow Visualization of Oscillating Heat Pipe by X-ray Imaging Method.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Shuhei Yoshida, Takurou Daimaru, Masahiro Kawaji, Hiroki Nagai
26.Effects of Check Valves on Thermal and Flow Characteristics of Oscillating Heat Pipes.[Proceedings of the 12th International Conference on Flow Dynamics,(2015)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai
27.Visualization of Loop Heat Pipe with Multiple Evaporators under Microgravity.[Proceedings of the 45th International Conference on Environmental Systems,(2015)]Hosei Nagano, Yuta Matsuda, Shun Okazaki, Hiroki Nagai, Hiroyuki Ogawa
28.Parametric Study of Oscillating Heat Pipes by using Mathematical Model for Practical Use in Spacecraft.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai, Atsushi Okamoto, Makiko Ando, Hiroyuki Sugita
29.Aerodynamic Characteristics of Airfoils with Different Aspect Ratio behind Propeller Slipstream in Low Reynolds Number Condition.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Kotaro Watanabe, Koji Fujita
30.Aerodynamic Challenge to Realize Mars Airplane.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Masayuki Anyoji, Taku Nonomura, Akira Oyama, Masato Okamoto, Gaku Sasaki, Takaaki Matsumoto, Kouichi Yonemoto, Kasahiro Kanazaki, Shigeru Sunada, Koichi Yonezawa, Masaru Koike, Koji Fujita, Keisuke Asai, Kozo Fujii
31.Development of Mars Exploration Aerial Vehicle in Japan.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hiroki Nagai, Akira Oyama, Mars Airplane WG
32.A Parametric Study of Mars Airplane Concept for Science Mission on Mars.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Koji Fujita, Hiroki Nagai, Akira Oyama
33.Development of an Oscillating Heat Pipe Cooling System for GAPS.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Hideyuki Fuke, Takayoshi Inoue, Akiko Kawachi, Daisuke Matsumoto, Yoshiro Miyazaki, Hiroki Nagai Taku Nonomura, Hiroyuki Ogawa, Naoki Yamada, et al
34.Conceptual Design Study of Oscillating Heat Pipe System for GAPS.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Shun Okazaki, Hideyuki Fuke, Takayoshi Inoue, Akiko Kawachi, Daisuke Matsumoto, Yoshiro Miyazaki, Hiroki Nagai Taku Nonomura, Hiroyuki Ogawa, Naoki Yamada
35.Experimental Study in Effects of Secondary Wick Configuration on Thermal Performance of a Loop Heat Pipe.[Proceedings of the 30th International Symposium on Space Technology and Science,(2015)]Masahiko Taketani, Takuya Adachi, Hiroki Nagai
36.Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel.[Journal of Visualization,18(2),(2015),297-309]M. Anyoji, D. Numata, H. Nagai, K. Asai
10.1007/s12650-014-0239-9
http://www.scopus.com/inward/record.url?eid=84940007053&partnerID=40
37.Aerodynamic Evaluation of a Capsule Shaped Projectile during Free Flight Testing with Ballistic Range.[AIAA SciTech 2015,(2015)]Akiho Ishida, Hiroki Nagai, Hideyuki Tanno, Tomoyuki Komoro
38.Operational characteristics of the oscillating heat pipe with noncondensable gas.[Journal of Thermophysics and Heat Transfer,29(3),(2015),563-571]Takurou Daimaru, Hiroki Nagai
10.2514/1.T4461
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000357940400014&DestApp=WOS http://www.scopus.com/inward/record.url?eid=84940737228&partnerID=40
39.Operational Characteristics of the Oscillating Heat Pipe with Non-Condensable Gas.[Journal of Thermophysics and Heat Transfer,29(3),(2015),563-571]Daimaru, T., Nagai, H.
10.2514/1.T4461 2015
40.The applications of pressure-sensitive paint in microfluidic systems.[Microfluid Nanofluid,18(5),(2015),739-753]Chih-Yung Huang, Yu Matsuda, James W. Gregory, Hiroki Nagai, Keisuke Asai
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