Presentation Information

1:40 PM - 2:00 PM JST(4:40 AM - 5:00 AM UTC)

[OS4-2-1-02]Inverse Design of Hypersonic Aircraft Using Surrogate Model based on Mode Decomposition

*Shun Takahashi¹, Takayuki Nagata², Kouichiro Tani¹, Masaru Koga¹, Tatsushi Isono¹, Masao Takegoshi¹, Sadatake Tomioka¹, Hiroyuki Kato³, Kota Tsukuda³, Daisuke Sasaki³ (1. Japan Aerospace Exploration Agency, 2. Nagoya University, 3. Osaka Metropolitan University)

Keywords:

Mode decomposition,Surrogate model,Hypersonic flow,Inverse design

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