[a-1] Intake and Nozzle

[2023-a-01] Experimental and Numerical Investigation of the Sideslip Angle Effect on the Ramjet Intake for High Mach Integrated Control Experiment (HIMICO) Model at Mach 2

*Yuki Kuwabara¹, Manami Fujii¹, Yuki Fujimori¹, Yusuke Hoshiya¹, Rintaro Tanaka¹, Shima Ariyoshi¹, Ayuto Suzuki¹, Tetsuya Sato¹, Hidemi Takahashi², Hideyuki Taguchi² (1. Waseda University, 2. JAXA)

キーワード：HIMICO, Intake, Sideslip angle, Wind tunnel test