著書論文等- 永井 大樹 -
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件数:705件
[2020]
21.[] A Feasibility Analysis of Collaborative Mission Using Mars Airplane and Mars Balloon - Mars Aerial-Exploration for Terrestrial and Tropospheric Environment Observation -.[TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN,18(3),(2020),64-70]Hiroto TANAKA, Issei MAMIYA, Hideki KIRITANI, Hiroki NAGASAWA, Takumi HIRATA, Tatsuya TONAI, Hiroki NAGAI, Koji FUJITA
10.2322/tastj.18.64
22.[] 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
23.[] Heat transfer performance of Pulsating Heat Pipe with Hydrofluoroolefin.[Transactions of the JSME (in Japanese),(2020)]Yosuke YASUDA, Fumika NABESHIMA, Sunao FUNAKOSHI, Hiroki NAGAI
10.1299/transjsme.20-00127
[2019]
24.[] 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
25.[] 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
26.[] 宇宙線反粒子探索GAPS実験計画の(特に日本チームの)現状報告.[大気球シンポジウム: 2019年度 = Balloon Symposium: 2019, (2019)]福家 英之, 小財 正義, 小川 博之, 岡崎 峻, 西城 大, 徳永 翔, 吉田 哲也, 中上 裕輔, 竹内 崇人, 和田 拓也, 吉田 篤正, 清水 雄輝, 山田 昇, 小池 貴久, 加藤 千尋, 宗像 一起, 永井 大樹, 五味 颯雅, 河内 明子, 小林 聖平, 近藤 愛実, 水野 広基, 長島 弘明, 高橋 俊, 竹村 薫, 田邉 拓哉, 井上 剛良, Hailey Charles, Perez Kerstin, Fabris Lorenzo, Craig William, Ong Rene, Boggs Steven, Doetinchem Philip von, Boezio Mirko, Fuke Hideyuki, Kozai Masayoshi, Ogawa Hiroyuki, Okazaki Shun, Saijo Masaru, Tokunaga Kakeru, Yoshida Tetsuya, Nakagami Yusuke, Takeuchi Shuto, Wada Takuya, Yoshida Atsumasa, Shimizu Yuki, Yamada Noboru, Koike Takahisa, Kato Chihiro, Munakata Kazuoki, Nagai Hiroki, Gomi Soga, Kawachi Akiko, Kobayashi Shohei, Kondo Manami, Mizuno Koki, Nagashima Hiroaki, Takahashi Shun, Takemura Kaoru, Tanabe Takuya, Inoue Takayoshi, Hailey Charles, Perez Kerstin, Fabris Lorenzo, Craig William, Ong Rene, Boggs Steven, Doetinchem Philip von, Boezio Mirko
27.[] 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
28.[] 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
29.[] Effects of rib number and rigid trailing edge on flexible-skinned thick wing at low reynolds number.[AIAA Scitech 2019 Forum, (2019)]Koji Fujita, Kenta Uechi, Koichi Takahashi, Hiroki Nagai
10.2514/6.2019-1893
http://www.scopus.com/inward/record.url?eid=85069004514&partnerID=40
30.[] 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
31.[] 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
32.[] 火星飛行機の実現に向けた空力課題への挑戦.[日本航空宇宙学会誌,67(6), (2019), 215-222]永井 大樹, 大山 聖, 安養寺 正之, 岡本 正人, 藤田 昂志, 米本 浩一
10.14822/kjsass.67.6_215
33.[] プロペラ後流中にある舵面を持つ翼の流れ場構造.[飛行機シンポジウム講演集(CD-ROM),56th, (2019), ROMBUNNO.3A11-]伊神翼, 藤田昂志, 永井大樹
10.2514/6.2019-2159
http://www.scopus.com/inward/record.url?eid=85068965801&partnerID=40
34.[] Reentry capsule dynamic instability with different aft-body shape in transonic flow.[AIAA Scitech 2019 Forum, (2019)]Masayuki Nomura, Arthur Robbe, Koji Fujita, Hiroki Nagai
10.2514/6.2019-0018
http://www.scopus.com/inward/record.url?eid=85068465200&partnerID=40
35.[] Experimental study on high efficiency of aerodynamic performance of rotor blades for mars helicopter.[AIAA Scitech 2019 Forum, (2019)]Kensuke Kanou, Koji Fujita, Hiroki Nagai
10.2514/6.2019-2160
http://www.scopus.com/inward/record.url?eid=85069004072&partnerID=40
36.[] Development of free flight experimental and analytical procedures for atmospheric entry vehicles.[AIAA Scitech 2019 Forum, (2019)]Olaseinde Jegede, Koji Fujita, Hiroki Nagai, Hideyuki Tanno
10.2514/6.2019-0019
http://www.scopus.com/inward/record.url?eid=85068468518&partnerID=40
37.[] 遷音速域における自由飛行カプセルの後流解析.[衝撃波シンポジウム講演論文集(CD-ROM),2018, (2019), ROMBUNNO.1A3‐2-]桐谷英樹, 永田貴之, 永井大樹, 大谷清伸, 小川俊広
[2018]
38.[] 低レイノルズ数における柔軟膜翼の風洞試験.[年会講演会講演集,49, (2018), 5p-]藤田 昂志, 上地 健太, 高橋 幸一, 永井 大樹
39.[] 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
40.[] 非定常PSP/TSP計測技術 (特集 PSP/TSP).[可視化情報学会誌 = Journal of the Visualization Society of Japan,38(148), (2018), 3-9,図巻頭1p]中北 和之, 杉岡 洋介, 永井 大樹
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