[G-1] Reusable Launch Vehicles (RLVs) 1

[2022-g-03] Flowfield visualization and mechanism of dynamic derivatives of a small-scale supersonic flight experiment vehicle being developed at Muroran Institute of Technology

*Shuuta Haraguchi¹, Shun Sasaki², Atsuya Honda¹, Ryuto Kawanabe², Haruka Nikado², Kazuhide Mizobata³ (1. Graduate student, Muroran-IT, 2. Undergraduate student, Muroran-IT, 3. Aerospace Plane Researth Center, Mutoran-IT)

キーワード：supersonic, flowfield visualization, dynamic derivatives, wind tunnel test