Knowledge Discovery for Transonic Regional-Jet Wing through Multidisciplinary Design Exploration by Kazuhisa CHIBA, Shigeru OBAYASHI, Hiroyuki MORINO

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Acquisition of Swept Aerodynamic Data by the Consecutive Changing of Wing Model Configuration in a Wind Tunnel Test Using Remote Feedback Control by Ken Wakimoto, Kazuhisa Chiba, Hiroyuki Kato, Kazuyuki Nakakita

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Remote and Feedback Control of the Flap Angle in a Wind Tunnel Test Model by Optical Measurement by Kazuhisa Chiba, Tatsuro Komatsu, Hiroyuki Kato, Kazuyuki Nakakita

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Diversity of design knowledge for launch vehicle in view of fuels on hybrid rocket engine by Kazuhisa CHIBA, Masahiro KANAZAKI, Masaki NAKAMIYA, Koki KITAGAWA, Toru SHIMADA

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Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics by Kazuhisa CHIBA, Shin'ya WATANABE, Masahiro KANAZAKI, Koki KITAGAWA, Toru SHIMADA

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