[S-3] Finalist Student Session3

[2023-g-19] Numerical Analysis and Wind Tunnel Testing of Experimental Reusable Vehicle RV-X Aerodynamics at 90° Angle-of-Attack

*Tomohiro Mamashita¹, Ryota Tamai², Tomotaro Muto², Keiichi Kitamura¹, Satoshi Nonaka³ (1. Yokohama National University, Department of Mechanical, Materials, and Ocean Engineering, 2. The University of Tokyo, Department of Aeronautics and Astronautics, 3. JAXA (Japan Aerospace Exploration Agency), Institute of Space and Astronautical Science)

Keywords:CFD, Reusable Launch Vehicle, Actual Flight Scale, High Angle-of-Attack Flow