論文- 永井 大樹 -
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件数:235件
[2009]
161.Oxygen-Sensing Properties of 5,10,15,20-Tetraphenylporphinato Platinum(II) and Palladium(II) Covalently Bound on Poly(isobutyl-co-2,2,2-trifluoroethyl methacrylate).[ounal of Polymer Science Part A, Polymer Chemistry,48(3),(2009),663-670]Makoto Obata, Noriko Matsuura, Kazunori Mitsuo, Hiroki Nagai, Keisuke Asai, Masafumi Harada, Shiho Hirohara, Masao Tanihara, Shigenobu Yano
[2008]
162.Experimental study on three-dimensional shock interference flow of a supersonic Busemann Biplane.[KSAS/JSASS Joint Int'l Symposium on Aerospace Engineering 2008,(2008)]OYAMA, S., NAGAI, H., ASAI, K.
163.Flow-induced vibration of a High-speed Train Running in a Tunnel.[KSAS/JSASS Joint Int'l Symposium on Aerospace Engineering 2008,(2008)]KODERA, T., NAGAI, H., ASAI, K., TERASHIMA, O.
164.Visualization of the heat flux distribution on a blunt-nosed body with an aerospike in hypersonic flow.[KSAS/JSASS Joint Int'l Symposium on Aerospace Engineering 2008,(2008)]HA, S. NAGAI, H., ASAI, K., NAKAKITA, K. and TSUBOI, N.
165.An experimental study of plasma actuator performance in martian atmospher.[5th International Conference on Flow Dynamics,(2008)]TAKAGAKI, M., NAGAI, H. and ASAI, K.
166.Design and construction of Mars Wind Tunnel for simulating atmospheric flight on Mars.[5th International Conference on Flow Dynamics,(2008)]ANYOJI, M., NAGAI, H. and ASAI, K.
167.PSP measurement of the leeward-side pressure distribution of a simplified car model in yaw.[5th International Conference on Flow Dynamics,(2008)]YORITA, D., NAGAI, H. and ASAI, K.
168.Luminescent Differential-Pressure Sensor Based on Gas Transfer through Porous Membrane.[13th International Symposium on Flow Visualization,(2008)]YORITA, D., NAGAI, H., ASAI, K..
169.Pressure-Sensitive Paint Measurement of Unsteady Pressure Field behind an Oscillating Fence Actuator.[13th International Symposium on Flow Visualization,(2008)]YAMASHITA, T., NAGAI, H., ASAI, K., SINGH, M. AND NAUGHTON, J. W.
170.Visualization of Interacting Flow Field between Busemann's Biplane in Supersonic Flow.[13th International Symposium on Flow Visualization,(2008)]KURATANI, N., NAGAI, H., ASAI, K., OGAWA, T., OBAYASHI, S.
171.Experimental Study on Interference Flow of a Supersonic Busemann Biplane using Pressure-Sensitive Paint Technique.[International Council of the Aeronautical Sciences 2008,(2008)]NAGAI, H., OYAMA, S., OGAWA, T., KURATANI, N., ASAI, K.
172.Evaluation of Plasma Actuator Performance in Martian Atmosphere for Applications to Mars Airplane.[38th Fluid Dynamics Conference,(2008)]TAKAGAKI, M., ISONO, S., NAGAI, H., ASAI, K.
173.Surface Pressure and Flow Field Behind an Oscillating Fence Submerged in Turbulent Boundary Layer.[26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference,(2008)]SINGH, M., NAUGHTON, J. W., YAMASHITA, T., NAGAI, H. and ASAI, K.
174.PSP measurement of Pressure Distribution in a Supersonic Micronozzle.[AIAA Journal,46,(2008),215-222]Nagai, H., Naraoka, R., Sawada,K., Asai, K.
175.Pressure-sensitive paint measurement of pressure distribution in a supersonic micronozzle.[AIAA Journal,46(1),(2008),215-222]H. Nagai, R. Naraoka, K. Sawada, K. Asai
10.2514/1.28371
http://www.scopus.com/inward/record.url?eid=38549163212&partnerID=40
176.Effect of Temperature-Sensitive Paint Thickness on Global Heat Transfer Measurement in Hypersonic Flow.[JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER,22,(2008),373-381]H. Nagai, S. Ohmi, K. Asai, K. Nakakita
177.Study on Thermal Performances of a Small Loop Heat Pipes.[Journal of Thermal Science and Technology,3,(2008),355-367]Hosei, NAGANO, Hiroki NAGAI, Fuyuko FUKUYOSHI, Hiroyuki OGAWA
http://ir.library.tohoku.ac.jp/re/handle/10097/51999
178.多孔質膜を用いた差圧応答型PSPの開発.[可視化情報学会論文集,28,(2008),21-26]依田大輔、永井大樹、浅井圭介
179.Study on Thermal Performances of a Small Loop Heat Pipe.[Journal of Thermal Science and Technology,3(2),(2008),355-367]NAGANO Hosei, NAGAI Hiroki, FUKUYOSHI Fuyuko, OGAWA Hiroyuki
10.1299/jtst.3.355
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000264830200016&DestApp=WOS
[2007]
180.Pressure-Sensitive Paint Measurement of the Flow around a Simplified Car Model.[Journal of Visualization,10(3),(2007),289-298]Yamashita,T., Sugiura, H., Nagai, H., Asai, K., Ishida, K.
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