著書論文等- 永井 大樹 -
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件数:679件
[2020]
1.[] 弾道飛行装置実験により自由飛行するカプセルの遷音速域における後流の時空間構造の特徴抽出.[2019年度衝撃波シンポジウム講演論文集, (2020)]桐谷英樹, 永井大樹, 藤田昂志, 大谷清伸
2.[] Blade Element Theory Coupled with CFD Applied to Optimal Design of Rotor for Mars Exploration Helicopter.[AIAA Scitech 2020 Forum, (2020)]Kazufumi Uwatoko, Masahiro Kanazaki, Hiroki Nagai, Koji Fujita, Akira Oyama
10.2514/6.2020-1284
3.[] 自由飛行するカプセルの遷音速領域における後流の時空間構造の特徴抽出解析.[令和元年度航空宇宙空力シンポジウム講演論文集, (2020)]永井大樹
4.[] Experimental and RANS analysis of full Mars airplane configurations.[AIAA Scitech 2020 Forum, (2020)]Shota Taniguchi, Akira Oyama, M Okamoto, Masato Okamoto, Masayuki Anyoji, Koji Fujita, Hiroki Nagai
10.2514/6.2020-2224
5.[] Parametric Study of Mars Helicopter for Pit Crater Exploration.[AIAA Scitech 2020 Forum, (2020)]Koji Fujita, Hilal Karaca, Hiroki Nagai
10.2514/6.2020-1734
6.[] Transonic Flow Field Analysis of a Free Flight Capsule using Ballistic Range.[AIAA Scitech 2020 Forum, (2020)]Hideki Kiritani, Naoki Tanaka, Kiyonobu Ohtani, Koji Fujita, Hiroki Nagai
10.2514/6.2020-1990
7.[] Deployable Wing Model Using ANCF and UVLM: Multibody Dynamic Simulation and Wind Tunnel Experiment.[AIAA Scitech 2020 Forum, (2020)]Keisuke Otsuka, Yinan Wang, Koji Fujita, Hiroki Nagai, Kanjuro Makihara
10.2514/6.2020-1678
8.[] 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]
9.[] 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
10.[] 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
11.[] 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
12.[] 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
13.[] 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
14.[] 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
15.[] 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
16.[] 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
17.[] 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
18.[] 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
19.[] 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
20.[] 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
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