[g-3] Flight Experiments 3

[2023-g-09] Flow Structure on Aerodynamics of a Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology

*Shun Sasaki¹, Shuta Haraguchi¹, Haruto Kita², Haruka Nikado¹, Ryuto Kawanabe², Kazuhide Mizobata³ (1. Muroran Institute of Technology, Guraduate Student, 2. Muroran Institute of Technology, Underguraduate Student, 3. Muroran Institute of Technology)

Keywords:supersonic, flowfield visualization, dynamic derivatives, wind tunnel test