論文- 永井 大樹 -
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件数:235件
[2007]
181.Thermal Performance of a Miniature Loop Heat Pipe for spacecraft thermal control system.[2007 ASME-JSME Thermal Engineering Summer Heat Transfer Conference,(2007)]Nagai, H., Nagano, H., Fukuyoshi, F., Ogawa, H.
182.Measurement of Oxygen Partial Pressure Distribution in Fuel Cell using Pressure-Sensitive Paint.[2007 ASME-JSME Thermal Engineering Summer Heat Transfer Conference,(2007)]Inagaki, S., Nagai, H. , Asai, K.
183.Evaluation of Lifetime-based Pressure-Sensitive Paint Measurement in Low-speed Flow.[22nd International Congress on Instrumentation in Aerospace Simulation Facilities,(2007)]Yamashita, T.,Nagai, H.,Asai, K.
184.Development of Pressure-Sensitive Paint Technique in a Supersonic Blowdown Wind Tunnel and its Application to a Busemann Biplane.[22nd International Congress on Instrumentation in Aerospace Simulation Facilities,(2007)]Saito, K., Ogawa, T., Nagai, H., Asai, K.
185.Visualization of Hypersonic Compression Corner Flows Using Temperature- and Pressure- Sensitive Paints.[45th AIAA Aerospace Science Meeting and Exhibit,(2007)]ISHIGURO, Y., OHMI, S., NAGAI, H., ASAI, K., NAKAKITA, K.
186.Unsteady Flow Measurements of a Slender Delta Wing in Wing Rock Motion.[45th AIAA Aerospace Science Meeting and Exhibit,(2007)]HIROSE, Y., NAGAI, H., KURASHINA, D., ASAI, K.
187.Pressure-sensitive paint measurement of the flow around a simplified car model.[Journal of Visualization,10(3),(2007),289-298]T. Yamashita, H. Sugiura, H. Nagai, K. Asai, K. Ishida
10.1007/BF03181696
http://www.scopus.com/inward/record.url?eid=38549091473&partnerID=40
188.Evaluation of lifetime-based Pressure-Sensitive Paint measurement in low-speed flow.[2007 22ND INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES,(2007),100-109]Taro Yamashita, Hiroki Nagai, Keisuke Asa
10.1109/ICIASF.2007.4380884
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000252358500012&DestApp=WOS http://www.scopus.com/inward/record.url?eid=51349129219&partnerID=40
189.Thermal performance of a miniature loop heat pipe for spacecraft thermal control system.[2007 Proceedings of the ASME/JSME Thermal Engineering Summer Heat Transfer Conference - HT 2007,3,(2007),721-726]Hiroki Nagai, Hosei Nagano, Fuyuko Fukuyoshi, Hiroyuki Ogawa
10.1115/HT2007-32805
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000254029800084&DestApp=WOS http://www.scopus.com/inward/record.url?eid=43449087643&partnerID=40
190.Measurement of oxygen partial pressure distribution in a fuel cell using pressure-sensitive paint.[2007 Proceedings of the ASME/JSME Thermal Engineering Summer Heat Transfer Conference - HT 2007,2,(2007),77-83]Suguru Inagaki, Hiroki Nagai, Keisuke Asai
10.1115/HT2007-32751
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000254072500011&DestApp=WOS http://www.scopus.com/inward/record.url?eid=43449096038&partnerID=40
[2006]
191.Molecular Sensors in Microturbine Measurement.[Proceedings of 2006 ASME International Mechanical Engineering Congress and Exposition,(2006)]HUANG, C.Y., Gregory, J. W., NAGAI, H., ASAI,K., Sullivan, J. P.
192.Application of Luminophore-Pendant Pressure-Sensitive Paint to Fluid Dynamic Measurements.[Proceedings of 12th International Symposium on Flow Visualization,(2006)]SAKAUE, H., MITSUO, K., IIJIMA, Y., MORITA, K., HYAKUTAKE, T., TAGUCHI, H., NISHIDE, H., KOJIMA, T., NAGAI, H., ASAI, K.
193.Flow Diagnostic using PSP and TSP technique in a Supersonic Micronozzle.[Proceedings of 12th International Symposium on Flow Visualization,(2006)]NAGAI, H., NARAOKA, R., SAWADA, K., ASAI, K.
194.PSP Measurement of the Flow around a Simplified Car Model.[Proceedings of 12th International Symposium on Flow Visualization,(2006)]Yamashita,T., Sugiura, H., Nagai, H., Asai, K., Ishida, K.
195.PSP measurement of Pressure Distribution in a Supersonic Micronozzle.[44th AIAA Aerospace Science Meeting and Exhibit,(2006)]NAGAI, H., NARAOKA, R., SAWADA, K., ASAI, K.
196.Application of Lifetime Imaging Method to a Cryogenic Wind Tunnel.[44th AIAA Aerospace Science Meeting and Exhibit,(2006)]KOJIMA, T., NAGAI, H., ASAI, K., MITSUO, K., IIJIMA, Y., SAKAUE, H.
197.Effect of TSP Layer Thickness on Global Heat Transfer Measurement in Hypersonic Flow.[44th AIAA Aerospace Science Meeting and Exhibit,(2006)]OHMI, S., NAGAI, H., ASAI, K., NAKAKITA, K.
198.Cryogenic Infrared Mission “JAXA/SPICA” with Advanced Cryocoolers.[Cryogenics,(2006)]H.Sugita, T. Nakagawa, H. Murakami, A. Okamoto, H. Nagai, M. Murakami, K. Narasaki, M. Hirabayashi, SPICA Working Group
[2005]
199.Thermal performance verification for the JEM MAXI Loop Heat Pipe and Radiator System.[Proceedings of 56th International Astronautical Congress,(2005)]Hiroki Nagai, Shiro Ueno
200.Innovative Cryogenic System for Japanese Infrared Astronomical Mission “SPICA”.[Proceedings of 56th International Astronautical Congress,(2005)]H. Sugita, T. Nakagawa, H. Murakami, T Matsumoto, H. Nagai, M. Murakami, K. Narasaki, M. Hirabayashi
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