[e-3] Atmospheric-entry (1)

[2023-e-11] Measurement of CO₂ Recombination Rates in Shock Tube with Divergent Nozzle

*Yoshihiro Shimizu¹, Satoshi Nomura², Hiroki Takayanagi², Masaya Matsuoka², Makoto Matsui¹, Kazuhisa Fujita² (1. Shizuoka Univ. Department of Mechanical Engineering, 2. Japan Aerospace Exploration Agency)

キーワード：Recombination Rate Coefficient , Carbon dioxide, Martian Atmospheric Entry, Nonequilibrium Flows