Koji Fujita
Koji Fujita
Institute of Fluid Science, Tohoku University
Verified email at tohoku.ac.jp - Homepage
TitleCited byYear
Simple and robust direct drive water power generation system using dielectric elastomers
S Chiba, M Waki, K Fujita, K Masuda, T Ikoma
Journal of Material Science and Engineering B 7, 1-2, 2017
102017
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), 449-468, 2017
92017
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
72012
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
52017
Conceptual Design of Mars Airplane
K Fujita, R Luong, H Nagai, K Asai
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2012
52012
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
42014
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
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
32016
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
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
22019
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
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
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
22014
火星探査航空機の初期概念検討
藤田昂志, R Luong, 永井大樹, 浅井圭介
平成 22 年度宇宙航行の力学シンポジウム, 2010
22010
Mars Airplane Conceptual Design
R Luong, 永井大樹, 浅井圭介, 藤田昂志
第 54 回宇宙科学技術連合講演会, 3F03, 静岡, 2010
22010
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
12019
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
12018
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
12018
火星飛行機の高高度飛行試験 (MABE-1) の概要
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, ...
年会講演会講演集 48, 8p, 2017
12017
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, ...
title 大気球シンポジウム: 平成 28 年度 Balloon Symposium: 2016, 2016
12016
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Articles 1–20