論文- 永井 大樹 -
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件数:235件
[2020]
1.Attitude Estimation using Thermopile Sensors on Mars Airplane Balloon Experiment-1 (MABE-1).[TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,18(2),(2020),17-24]TOKUTAKE Hiroshi, FUJITA Koji, OYAMA Akira, NAGAI Hiroki
10.2322/tastj.18.17
[2019]
2.Aerodynamic performance of control surfaces on mars airplane balloon experiment two.[Journal of Fluid Science and Technology,14(3),(2019),JFST0017]Masahiro Kanazaki, Kai Tomisawa, Koji Fujita, Akira Oyama, Hiroki Nagai
10.1299/jfst.2019jfst0017
http://www.scopus.com/inward/record.url?eid=85078819452&partnerID=40
3.Numerical study of temperature oscillation in loop heat pipe.[Applied Thermal Engineering,163,(2019)]Takuya Adachi, Koji Fujita, Hiroki Nagai
10.1016/j.applthermaleng.2019.114281
http://www.scopus.com/inward/record.url?eid=85071866128&partnerID=40
4.The Quantitative Density Measurement of Unsteady Flow around the Projectile.[Journal of Flow Control, Measurement & Visualization,(2019),111-119]Yusuke Hirose, Kazuki Ishikawa, Yoshiyuki Ishimoto, Takumi Nagashima, Masanori Ota, Shinsuke Udagawa, Tatsuro Inage, Kazuki Fujita, Hideki Kiritani, Koji Fujita, Kiyonobu Ohtani, Hiroki Nagai
10.4236/jfcmv.2019.72009
5.Wind Tunnel Test for Videogrammetric Deformation Measurement of UAV for Mars Airplane Balloon Experiment-1 (MABE-1)*.[Journal of Flow Control, Measurement & Visualization,(7),(2019),87-100]Koji Fujita, Akira Oyama, Daisuke Kubo, Masahiro Kanazaki, Hiroki Nagai
6.Multifidelity modeling of deployable wings: Multibody dynamic simulation and wind tunnel experiment.[AIAA Journal,57(10),(2019),4300-4311]Keisuke Otsuka, Yinan Wang, Koji Fujita, Hiroki Nagai, Kanjuro Makihara
10.2514/1.J058676
http://www.scopus.com/inward/record.url?eid=85078540555&partnerID=40
7.Flight Control Parameter Design for Mars Airplane Balloon Experiment-1 (MABE-1) Using Evolutionary Computation.[TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,17(4),(2019),512-518]FUJITA Koji, TOKUTAKE Hiroshi, NAGAI Hiroki, OYAMA Akira
10.2322/tastj.17.512
[2018]
8.On-orbit demonstration of oscillating heat pipe with check valves for space application.[Applied Thermal Engineering,130,(2018),552-560]Makiko Ando, Atsushi Okamoto, Kosuke Tanaka, Masakatsu Maeda, Hiroyuki Sugita, Takurou Daimaru, Hiroki Nagai
10.1016/j.applthermaleng.2017.11.032
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000424177600051&DestApp=WOS http://www.scopus.com/inward/record.url?eid=85036610109&partnerID=40
9.Computational study of aerodynamic characteristics on reentry capsule aft-body shape in transonic flow.[AIAA Atmospheric Flight Mechanics Conference, 2018,(209999),(2018)]Masayuki Nomura, Koji Fujita, Hiroki Nagai
10.2514/6.2018-0290
http://www.scopus.com/inward/record.url?eid=85044369463&partnerID=40
[2017]
10.Robustness analysis on aerial deployment motion of a Mars aircraft using multibody dynamics simulation: Effects of wing-unfolding torque and timing.[Aeronautical Journal,121(1238),(2017),449-468]Koji Fujita, Hiroki Nagai
10.1017/aer.2016.123
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000415149700002&DestApp=WOS http://www.scopus.com/inward/record.url?eid=85017449141&partnerID=40
11.Operating Characteristics of Loop Heat Pipe With Two Evaporators and Two Condensers under atmospheric condition.[Proceedings of Asian Conference on Thermal Science 2017,(2017)]X. Chang, H. Nagano, S. Okazaki, H. Ogawa, H. Nagai
12.Study on thermal cycle in oscillating heat pipes by numerical analysis.[Applied Thermal Engineering,113,(2017),1219-1227]Takurou Daimaru, Shuhei Yoshida, Hiroki Nagai
10.1016/j.applthermaleng.2016.11.114
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000394723300116&DestApp=WOS http://www.scopus.com/inward/record.url?eid=84997217075&partnerID=40
13.Global Heat Flux Measurement Using Temperature-Sensitive Paint in High-Enthalpy Shock Tunnel HIEST.[Proceedings of AIAA SciTech2017,(2017)]T. Nagayama, H. Nagai, H. Tanno, T. Komuro
14.Study on Thermal Cycle in Oscillating Heat Pipe by Numerical Analysis.[Applied Thermal Engineering,113(25),(2017),1219-1227]T. Daimaru, S. Yoshida, H. Nagai
15.Comparison between numerical simulation and on-orbit experiment of oscillating heat pipes.[International Journal of Heat and Mass Transfer,109,(2017),791-806]T. Daimaru, H. Nagai, M. Ando, K. Tanaka, A. Okamoto, H. Sugita
16.Robustness Analysis on Aerial Deployment Motion of a Mars Airplane using Multibody Dynamics Simulation: Effects of Wing-Unfolding Torque and Timing.[The Aeronautical Journal,(2017)]K. Fujita, H. Nagai
17.Ultrafast-response anodized-Aluminum pressure-sensitive paints for unsteady flow measurement.[AIAA Journal,55(4),(2017),1118-1125]Daiju Numata, Shota Fujii, Hiroki Nagai, Keisuke Asai
10.2514/1.J054886
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000400284700003&DestApp=WOS http://www.scopus.com/inward/record.url?eid=85017186618&partnerID=40
18.Characterization of frequency response of pressure-sensitive paints.[AIAA Journal,55(4),(2017),1460-1464]Tamao Sugimoto, Yosuke Sugioka, Daiju Numata, Hiroki Nagai, Keisuke Asai
10.2514/1.J054985
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000400284700031&DestApp=WOS http://www.scopus.com/inward/record.url?eid=85017107281&partnerID=40
19.Comparison between numerical simulation and on-orbit experiment of oscillating heat pipes.[International Journal of Heat and Mass Transfer,109,(2017),791-806]Takurou Daimaru, Hiroki Nagai, Makiko Ando, Kosuke Tanaka, Atsushi Okamoto, Hiroyuki Sugita
10.1016/j.ijheatmasstransfer.2017.01.078
http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=TohokuUniv&SrcApp=TohokuUniv&DestLinkType=FullRecord&KeyUT=WOS:000400227300072&DestApp=WOS http://www.scopus.com/inward/record.url?eid=85014007741&partnerID=40
20.Evaluation of Aerodynamic Performance of Mars Airplane in Scientific Balloon Experiment.[Fluid Mechanics Research International Journal,1(3),(2017)]Masayuki Anyoji, Masato Okamoto, Koji Fujita, Hiroki Nagai, Akira Oyama
10.15406/fmrij.2017.01.00012
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