[C-2] Structural Dynamics and Control

[2022-c-07] Experimental Studies of Sloshing Dynamics for the Tank with Hemispheric Diaphragm

*Taro Kawano¹, Nobukatsu Okuizumi², Hikaru Eguchi³, Keisuke Michigami¹, Hitoshi Hamori¹, Susumu Yasuda¹, Rie Tagai¹, Shujiro Sawai² (1. Japan Aerospace Exploration Agency, Research and Development Directorate, 2. Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, 3. Muroran Institute of Technology, Aerospace Plane Research Center)

キーワード：Sloshing, Diaphragm Tank, SLIM, Lander