論文- 永井 大樹 -
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件数:232件
[2011]
121.Unsteady Aerodynamic Experiment of NACA0012 Airfoil at Low Reynolds Number.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011)]Nose, K., Sakai, N., Numata, D., Nagai, H., Asai, K., Ikeda, T. and Atobe, T.
122.High-accuracy Calculation for Aerodynamic Heating Using Temperature-Sensitive Paint.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),552-553]Nishigata, K., Sawamura, R., Nagai, H., and Asai, K.
123.Development of Temperature-Sensitive Paint for High-Temperature Measurement.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),558-559]Sawamura, R., Nishigata, K., Nagai, H., and Asai, K.
124.Heat Transfer Characteristics of Oscillating Heat Pipe by Difference of Surface Characteristic.[Proceedings of the Eighth International Conference on Flow Dynamics,(2011),556-557]Kanayama, T., Daimaru, T., Nagai, H., Ogawa, H.
125.Development of an experimental small loop heat pipe with polytetrafluoroethylene wicks.[Journal of Thermophysics and Heat Transfer,25,(2011),547-552]Hosei Nagano, Fuyuko Fukuyoshi, Hiroyuki Ogawa, Hiroki Nagai
10.2514/1.T3614
http://www.scopus.com/inward/record.url?eid=80054077357&partnerID=40
126."SUPERSONIC WIND TUNNEL EXPERIMENT ON AERODYNAMIC CHARACTERISTICS AND WINGLETS EFFECTS OF THE TAPERED SUPERSONIC BIPLANE.[AJK2011-15015, Proceedings of ASME-JSME-KSME Joint Fluids Engineering Conference 2011, AJK2011-FED,(2011)]Fujisono, T., Yamashita, H., Toyoda, A., Nagai, H., Asai, K., Matsuno, T., Kawazoe, H., Jeong, S. and Obayashi, S.
127.PSP Measurement of Pressure Distribution on a Cambered Airfoil for Mars Exploration Airplane.[Proceedings of the 11th Asian Symposium on Visualization,(2011)]Nose, K., Anyoji, M., Numata, D., Nagai, H. and Asai, K.
128.Evaluation of Transfer Function of Pressure-Sensitive Paint for Unsteady Flow Measurement.[Proceedings of the 11th Asian Symposium on Visualization,(2011)]T. Sugimoto, D. Yorita, D. Numata, H. Nagai, K. Asai
129.Evaluation of Temperature-Sensitive Paint using Thermographic Phosphor by Hypersonic Aerodynamic Heating.[Proceedings of the 11th Asian Symposium on Visualization,(2011)]Sawamura, R., Nishigata, K., Nagai, H., Asai, K.
130.Surface pressure and flow field behind an oscillating fence submerged in turbulent boundary layer.[Experiments in Fluids,50(3),(2011),701-714]Manjinder Singh, Jonathan W. Naughton, Taro Yamashita, Hiroki Nagai, Keisuke Asai
10.1007/s00348-010-0977-y
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000287584300016&DestApp=WOS http://www.scopus.com/inward/record.url?eid=79954573462&partnerID=40
131.Surface Pressure and Flow Field Behind an Oscillating Fence Submerged in a Turbulent Boundary Layer, Experiments in Fluids.[Experiments in Fluids,(2011),701-714]Singh, M., Naughton, J.W., Yamashita, T., Nagai, H., Asai, K.
0.1007/s00348-010-0977-y
132.Development of a Low-Density Wind Tunnel for Simulating Martian Atmospheric Flight.[AEROSPACE TECHNOLOGY JAPAN,9,(2011),21-27]Masayuki ANYOJI, Kei NOSE, Shingo IDA, Daiju NUMATA, Hiroki NAGAI and Keisuke ASAI
[2010]
133.Development of Aerodynamic Heating Measurement Technique Using Temperaturesensitive Paint in Hypersonic Flow.[The 14th International Symposium on Flow Visualization,(2010)]Ha, S., Sawamura, R., Nagai, H., Asai, K.
134.Measuring Unsteady Low-Speed Flow Phenomena by Using a Time-Series Analysis of Pressure-Sensitive Paint Images.[The 14th International Symposium on Flow Visualization,(2010)]Yorita, D., Numata, D., Nagai, H., Asai, K.
135.Visualization of a Three-Dimensional Shock-Wave Structures in a Supersonic Busemann Biplane by Sharp Focusing Schlieren System and PSP Measurement.[The 14th International Symposium on Flow Visualization,(2010)]Hagiwara, M., Nagai, H., Numata, D., Asai, K.
136.Imaging Measurement of Skin Friction Field around Bluff Body Using Luminescent Oil Film Technique.[The 14th International Symposium on Flow Visualization,(2010)]Kakuta, T., Koyama, A., Yorita, D., Numata, D., Nagai, H., Asai, K., Woodiga, S.A., Liu, T.
137.Development of Pressure-Sensitive Paint Technique for Surface Pressure Measurement in a Mars Wind Tunnel.[The 14th International Symposium on Flow Visualization,(2010)]Ono, T., Anyoji, M., Ida, S., Nose, K., Numata, D., Nagai, H., Asai, K.
138.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).[Journal of Polymer Science, Part A: Polymer Chemistry,48(3),(2010),663-670]Makoto Obata, Noriko Matsuura, Kazunori Mitsuo, Hiroki Nagai, Keisuke Asai, Masafumi Harada, Shiho Hirohara, Masao Tanihara, Shigenobu Yano
10.1002/pola.23818
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000274254600018&DestApp=WOS http://www.scopus.com/inward/record.url?eid=75749150185&partnerID=40
139.Experimental Study on Dynamic Instability of Re- Entry Capsule-Shaped Body using Pressure- Sensitive Paint.[48th AIAA Aerospace Science Meeting and Exhibit,(2010)]SUGIMOTO, D., NAGAI, H., ASAI, K., HIRAKI, K.
140.Experimental Study of Heat Transfer Measurement using Temperature-Sensitive Paint for High-Temperature Application in Hypersonic Flow.[49th AIAA Aerospace Science Meeting and Exhibit,(2010)]Hiroki Nagai, Ryosuke Sawamura and Keisuke Asai
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