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Shintaro Shigeoka
Shintaro Shigeoka
Kyushu Institute of Technology
Reynolds number
Physics
Mechanics
Aerospace engineering
Supersonic wind tunnel
4
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2
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0
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807 Cluster Analysis of Shape Parameters of High Lift-to-Drag Ratio Low Reynolds Number Airfoils
2014
Shintaro Shigeoka
Gaku Sasaki
Takaaki Matsumoto
Koichi Yonemoto
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510 Performance Validation of Optimal Airfoils for Low Reynolds Number Flow Using Variable-pressure Wind Tunnel
2013
Shintaro Shigeoka
Gaku Sasaki
Hiroshi Ochi
Koichi Yonemoto
Takaaki Matsumoto
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Design, development and flight experiment of a small reusable rocket that glides using two-stage parachute
2011
SII | IEEE/SICE International Symposium on System Integration
Kyoshiro Itakura
Takahiro Kobayashi
Gaku Sasaki
Koki Ishibashi
Shintaro Shigeoka
Masahiro Sugii
Naoya Ueta
Yuki Nakachi
Yuta Nakayama
Sachi Inai
Tomohiro Narumi
Takaaki Matsumoto
Shinichi Sagara
Yasuhiro Akahoshi
Toshiaki Kanemoto
Koichi Yonemoto
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C24 About Aspect Ratio Study on Three-Dimensional Wing at Low Reynolds Number Flow Using Variable-Pressure Wind Tunnel
2011
Shintaro Shigeoka
Hiroshi Ochi
Koichi Yonemoto
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