Presentation Information

9:30 AM - 9:50 AM JST(12:30 AM - 12:50 AM UTC)

[OS3-3-3-02]Investigation of the Vibration Damping Mechanism of a Thin-Shell Aeroshell in the Subsonic Regime by 1DOF Free Vibration Analysis

*Ren Momoi^1,2, Takeshi Sawada^3,2, Ryoki Chokawa^4,2, Takashi Aoyama², Akira Oyama², Masahiro Kanazaki⁴, Koji Miyaji¹ (1. Yokohama National University, 2. JAXA, 3. Tokyo University , 4. Tokyo Metropolitan University)

Keywords:

Thin-Shell Aeroshel,one-degree-of-freedom oscillation analysis

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