Koji Fujita
Koji Fujita
Institute of Fluid Science, Tohoku University
Verified email at tohoku.ac.jp - Homepage
Title
Cited by
Cited by
Year
Robustness analysis on aerial deployment motion of a Mars aircraft using multibody dynamics simulation: effects of wing-unfolding torque and timing
K Fujita, H Nagai
The Aeronautical Journal 121 (1238), 449, 2017
122017
Conceptual design of a miniature, propeller-driven airplane for Mars
K Fujita, H Nagai, K Asai
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
122012
Simple and robust direct drive water power generation system using dielectric elastomers
S Chiba, M Waki, K Fujita, K Masuda, T Ikoma
J Mater Sci Eng B 7, 1-2, 2017
112017
Conceptual Design of Mars Airplane
K Fujita, R Luong, H Nagai, K Asai
Transactions of the Japan Society for Aeronautical and Space Sciences …, 2012
82012
Comparing aerial-deployment-mechanism designs for Mars airplane
K Fujita, H Nagai
Transactions of the Japan Society for Aeronautical and Space Sciences 59 (6 …, 2016
72016
Innovative elastomer transducer driven by Karman vortices in water flow
S Chiba, K Hasegawa, M Waki, K Fujita, K Ohyama, S Zhu
J Mater Sci Eng A 7 (5-6), 121-35, 2017
62017
A parametric study of Mars airplane concept for science mission on Mars
K Fujita, H Nagai, A Oyama
Transactions of the Japan Society for Aeronautical and Space Sciences …, 2016
62016
Dynamic behaviour of Mars airplane with folded-wing deployment
K FUJITA, T MOTODA, H NAGAI
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2014
52014
Conceptual Helicopter Design for Exploration of Pit Craters and Caves on Mars
R Aoki, A Oyama, K Fujita, H Nagai, M Kanazaki, K Kanou, N Inoue, ...
2018 AIAA SPACE and Astronautics Forum and Exposition, 5362, 2018
42018
Aerodynamic Characteristics of Mars Airplane Airfoils with Control Surface in Propeller Slipstream
K Kurane, K Uechi, K Takahashi, K Fujita, H Nagai
2018 AIAA Aerospace Sciences Meeting, 2058, 2018
42018
MELOS1 にむけた火星飛行機の高高度飛行試験計画
大山聖, 永井大樹, 竹内伸介, 豊田裕之, 藤田昂志, 安養寺正之, ...
第 56 回宇宙科学技術連合講演会, 2E01, 2012
42012
Flight control parameter design for Mars airplane balloon experiment-1 (MABE-1) using evolutionary computation
K FUJITA, H TOKUTAKE, H NAGAI, A OYAMA
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2019
32019
高高度飛行試験による火星飛行機の空力データの取得
大山聖, 永井大樹, 得竹浩, 藤田昂志, 安養寺正之, 豊田裕之, 宮澤優, ...
宇宙航空研究開発機構研究開発報告: 大気球研究報告, 69-80, 2017
32017
A Parametric study of the deployable wing airplane for Mars exploration
K Fujita
Proceedings of the 29th Congress of the International Council of the …, 2014
32014
Numerical analysis for an aerial deployment motion of a folded-wing airplane
K Fujita, T Motoda, H Nagai
AIAA Atmospheric Flight Mechanics Conference, 0383, 2014
32014
Recent progress on soft transducers for sensor networks
S Chiba, M Waki, K Fujita, Z Song, K Ohyama, S Zhu
Technologies and Eco-innovation towards Sustainability II, 285-298, 2019
22019
Development of Free Flight Experimental and Analytical Procedures for Atmospheric Entry Vehicles
O Jegede, K Fujita, H Nagai, H Tanno
AIAA Scitech 2019 Forum, 0019, 2019
22019
Flow Field on Wing Surface with Control Surface in Propeller Slipstream at Low Reynolds Number
T Ikami, K Kanou, K Takahashi, K Fujita, H Nagai
AIAA Scitech 2019 Forum, 2159, 2019
22019
Robust aerial deployment of Mars airplane with tilted folding-axis
K Fujita, H Nagai, A Oyama
AIAA Atmospheric Flight Mechanics Conference, 0023, 2016
22016
Aerodynamic Characteristics of Airfoils with Different Aspect Ratio behind Propeller Slipstream in Low Reynolds Number
H Nagai, K Watanabe, K Fujita
30th International Symposium on Space Technology and Science, Kobe-Hyogo, Japan, 2015
22015
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Articles 1–20