Presentaion at conference, meeting, etc. - MIZOBATA Kazuhide
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Flow Structure on Aerodynamics of a Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
Shun SASAKI, Shuta HARAGUCHI, Haruto KITA, Haruka NIAKDO, Ryuto KAWANABE, and Kazuhide MIZOBATA,The 34th International Symposium on Space Technology and Science (ISTS),(一社)日本航空宇宙学会,Preprints of 34th International Symposium on Space Technology and Science (ネット公開),2023.06.03,Kurume,Japan
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Flowfield Visualization and Mechanism of Dynamic Derivatives of a Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
Shuuta HARAGUCHI, Shun SASAKI, Atsuya HONDA, Ryuto KAWANABE, Haruka NIKADO, Kazuhide MIZOBATA,33rd International Symposium on Space Technology and Science,(一社)日本航空宇宙学会,Preprints of 33rd International Symposium on Space Technology and Science (ネット公開),2022.02.26,リモート開催,Japan
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Drag Reduction of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology (Third Report)
Tomohiro SHIGEKIYO, Nana HASEGAWA, Katsuya MIYAMOTO, Kazuhide MIZOBATA,33rd International Symposium on Space Technology and Science,(一社)日本航空宇宙学会,Preprints of 33rd International Symposium on Space Technology and Science (ネット公開),2022.02.26,リモート開催,Japan
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Aerodynamic Characteristics of a Rocket-Based Combined Cycle Spaceplane
Yoshimasa Nishimura, Kazuhide Mizobata, Susumu Hasegawa, Kanenori Kato, Kouichiro Tani, and Takeshi Kanda,32nd International Symposium on Space Technology and Science, June 15-21, Fukui Japan,(一社)日本航空宇宙学会,Preprints of 32nd International Symposium on Space Technology and Science,2019.06,Fukui,Japan
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Aerodynamics Caused by Attitude Rates of a Supersonic Flight Experiment Vehicle with a Cranked-arrow Main Wing
Kazuhide Mizobata, Yukiya Ishigami, Masaaki Miura, Keisuke Shiono, Koji Shirakata, Akihiro Nishida, and Atsuya Honda,32nd International Symposium on Space Technology and Science, June 15-21, Fukui Japan,(一社)日本航空宇宙学会,Preprints of 32nd International Symposium on Space Technology and Science,2019.06,Fukui,Japan
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Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology (Second Report)
Taichi Mio, Katsuya Miyamoto, Yuki Yamazaki, and Kazuhide Mizobata,32nd International Symposium on Space Technology and Science, June 15-21, Fukui Japan,(一社)日本航空宇宙学会,Preprints of 32nd International Symposium on Space Technology and Science,2019.06,Fukui,Japan
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Aerodynamic Derivatives with Respect to Pitching and Yawing Rates of a Small-scale Supersonic Flight Experiment Vehicle
Keisuke Shiono, Koji Shirakata, Yukiya Ishigami, Masaaki Miura, Kazuhide Mizobata, Kazuyuki Higashino, and Takakage Arai,31st International Symposium on Space Technology and Science, Matsuyama, Japan, June 3-9, 2017,Japan Society for Aeronautical and Space Sciences,Preprints of the 31st ISTS,2017.06.07,Matsuyama,Japan
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Aerodynamics Caused by Rolling Rates of a Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
Kazuhide Mizobata, Yukiya Ishigami, Masaaki Miura, Kazuyuki Higashino, and Takakage Arai,31st International Symposium on Space Technology and Science, Matsuyama, Japan, June 3-9, 2017,Japan Society for Aeronautical and Space Sciences,Preprints of the 31st ISTS,2017.06.07,Matsuyama,Japan
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Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
Yuki Yamazaki, Kazuhide Mizobata, and Kazuyuki Higashino,31st International Symposium on Space Technology and Science, Matsuyama, Japan, June 3-9, 2017,Japan Society for Aeronautical and Space Sciences,Preprints of the 31st ISTS,2017.06.07,Matsuyama,Japan
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Some Recent Aerodynamic Treatments for a Supersonic Flight Experiment Vehicle with a Cranked-arrow Main Wing Being Developed at Muroran Institute of Technology
Kazuhide MIZOBATA, Yukiya ISHIGAMI, Masaaki MIURA, Keisuke SHIONO, Yuki YAMAZAKI, Kazuyuki HIGASHINO, and Takakage ARAI,The 2016 Asia-Pacific International Symposium on Aerospace Technology,Preprints of the 2016 Asia-Pacific International Symposium on Aerospace Technology,2016.10.25,Toyama,Japan
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Aerodynamics Caused by Rolling Motion of a Small-scale Supersonic Flight Experiment Vehicle
Yukiya Ishigami, Masaaki Miura, Kazuhide Mizobata, Kazuyuki Higashino, and Takakage Arai,The 2016 Asia-Pacific International Symposium on Aerospace Technology,Preprints of the 2016 Asia-Pacific International Symposium on Aerospace Technology,2016.10.25,Toyama,Japan
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Aerodynamics Caused by Rolling Motion of a Supersonic Flight Experiment Vehicle with a Cranked-arrow Main Wing
K. Mizobata, Y. Ishigami, Y. Suzuki, K. Higashino, and T. Arai,2015 Asia-Pacific International Symposium on Aerospace Technology,Societies of Aeronautics and Astronautics in Japan, Korea, Chine, and Australia,2015 Asia-Pacific International Symposium on Aerospace Technology,2015.11,Cairns,Australia
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Aerodynamics and Flight Capability of a Supersonic Flight Experiment Vehicle
Kazuhide MIZOBATA, Yoshihiro Suzuki, Sakae Ooishi, Satoshi Kondoh, Tsubasa Toguchi, Yukiya Ishigami, Masaaki Miura, Takakage Arai, and Kazuyuki Higashino,30th International Symposium on Space Technology and Science,Japan Society for Aeronautical and Space Sciences,30th International Symposium on Space Technology and Science,2015.07,Kobe,Japan
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DEVELOPMENT OF A SMALL-SCALE SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED
Kazuhide Mizobata, Ryojiro Minato, Ken Higuchi, Masazumi Ueba, Syohei Takagi, Daisuke Nakata, Nobuhisa Katsumata, Kazuyuki Higashino, and Nobuhiro Tanatsugu,29th Congress of the International Council of the Aeronautical Sciences,The International Council of the Aeronautical Sciences,29th Congress of the International Council of the Aeronautical Sciences,2014.09,St. Petersburg,Russian Federation
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Aerodynamic Characterization of a Small-Scale Supersonic Flight Experimental Vehicle with a Cranked-Arrow Main Wing and Tails by Wind-Tunnel and Flight Tests
Kazuhide Mizobata, Ryojiro Minato, Kazuyuki Higashino, and Nobuhiro Tanatsugu,2013 Asia-Pacific International Symposium on Aerospace Technology,Societies of Aeronautics and Astronautics in Japan, Korea, Chine, and Australia,2013 Asia-Pacific International Symposium on Aerospace Technology,2013.11,Takamatsu,Japan
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Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed for Future Space Transportation Research
Kazuhide Mizobata, Ryojiro Minato, Ken Higuchi, Masazumi Ueba, Syohei Takagi, Daisuke Nakata, Kazuyuki Higashino, and Nobuhiro Tanatsugu,29th International Symposium on Space Technology and Science,Japan Society for Aeronautical and Space Sciences,29th International Symposium on Space Technology and Science,2013.06,Nagoya,Japan
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Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed
Kazuhide MIZOBATA,28th International Congress of the Aeronautical Sciences,The International Council of the Aeronautical Sciences,ICAS 2012 CD-ROM Proceedings,2012.09,Brisbane,Australia
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室蘭工大の小型超音速飛行実験機にかかる空力研究の現況について(その2)
溝端一秀,第56回流体力学講演会,(一社)日本航空宇宙学会,第56回流体力学講演会講演集(ダウンロード版),2024.07.03,鹿児島市,Japan
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室蘭工大小型超音速飛行実験機の遷音速風試における底面抗力の評価
重清智大,高橋直希,溝端一秀,令和4年度宇宙輸送シンポジウム,(国研)宇宙航空研究開発機構・宇宙科学研究所,予稿集無し,2023.01.12,相模原市
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航空宇宙機の推進空力統合風試におけるエンジン噴射模擬のためのインフレータ利用可能性
小林武史,小笠原直哉,溝端一秀,令和4年度宇宙輸送シンポジウム,(国研)宇宙航空研究開発機構・宇宙科学研究所,予稿集無し,2023.01.12,相模原市