[2023-a-02]Experimental and Numerical Investigation of a Three-Dimensional Supersonic Inlet for the Reusable Sounding Rocket with ATRIUM Engine
*Kazuma Matsumoto1, Haruaki Seta1, Daiki Watanabe1, Yusuke Maru2, Tetsuya Sato1(1. Waseda Univ. Department of Applied Mechanics and Aerospace Engineering, 2. JAXA Institute of Space and Astronautical Science)
Keywords:
Supersonic Inlet,Wind Tunnel Test,CFD,Air-breathing Engine,Reusable Sounding Rocket
